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This commit is contained in:
Damjan Adamic 2014-05-05 22:13:24 +02:00
parent b9ee1d5dee
commit 61addd3d4e
42 changed files with 1291 additions and 1185 deletions
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5
DONATIONS.txt
View file

@ -133,7 +133,7 @@ Eric Burdis
Nigel Chippindale
Michael Deasy
Stephen Stough
Kenneth Lilja
Kenneth Lilja (monthly)
Robert Jero
Gary Bancroft
Robert Cotsford
@ -386,3 +386,6 @@ Wilco Hijink
Roy Nixon
Lexington S Morley
Daryl Dacko
Beat Zurflueh
Piotr Kundu
Kevin Berkefeld

60
companion/src/comparedialog.cpp
View file

@ -76,7 +76,7 @@ void CompareDialog::printDiff()
{
te->clear();
printSetup();
if (GetCurrentFirmware()->getCapability(FlightPhases)) {
if (GetCurrentFirmware()->getCapability(FlightModes)) {
printPhases();
}
printExpos();
@ -309,7 +309,7 @@ void CompareDialog::printPhases()
str.append(QString("<td width=\"40\" align=\"center\"><b>%1</b></td>").arg(getInputStr(*g_model1, i)));
}
str.append("</tr>");
for (i=0; i<GetCurrentFirmware()->getCapability(FlightPhases); i++) {
for (i=0; i<GetCurrentFirmware()->getCapability(FlightModes); i++) {
PhaseData *pd1=&g_model1->phaseData[i];
PhaseData *pd2=&g_model2->phaseData[i];
str.append("<tr><td><b>"+tr("FM")+QString("%1</b> ").arg(i));
@ -346,10 +346,10 @@ void CompareDialog::printPhases()
if (gvars==1) {
gvarnum=GetCurrentFirmware()->getCapability(Gvars);
}
if ((gvars==1 && GetCurrentFirmware()->getCapability(GvarsFlightPhases)) || GetCurrentFirmware()->getCapability(RotaryEncoders)) {
if ((gvars==1 && GetCurrentFirmware()->getCapability(GvarsFlightModes)) || GetCurrentFirmware()->getCapability(RotaryEncoders)) {
str.append("<br><table border=1 cellspacing=0 cellpadding=1 width=\"100%\">");
str.append("<tr><td style=\"border-style:none;\">&nbsp;</td>");
if (GetCurrentFirmware()->getCapability(GvarsFlightPhases)) {
if (GetCurrentFirmware()->getCapability(GvarsFlightModes)) {
str.append(QString("<td colspan=%1 align=center><b>").arg(gvarnum)+tr("Gvars")+"</td>");
}
@ -357,7 +357,7 @@ void CompareDialog::printPhases()
str.append(QString("<td colspan=%1 align=center><b>").arg(GetCurrentFirmware()->getCapability(RotaryEncoders))+tr("Rot. Enc.")+"</td>");
}
str.append("</tr><tr><td align=center><b>"+tr("Flight mode name")+"</b></td>");
if (GetCurrentFirmware()->getCapability(GvarsFlightPhases)) {
if (GetCurrentFirmware()->getCapability(GvarsFlightModes)) {
for (i=0; i<gvarnum; i++) {
str.append(QString("<td width=\"40\" align=\"center\"><b>GV%1</b><br>%2</td>").arg(i+1).arg(g_model1->gvars_names[i]));
}
@ -366,13 +366,13 @@ void CompareDialog::printPhases()
str.append(QString("<td align=\"center\"><b>RE%1</b></td>").arg((i==0 ? 'A': 'B')));
}
str.append("</tr>");
for (i=0; i<GetCurrentFirmware()->getCapability(FlightPhases); i++) {
for (i=0; i<GetCurrentFirmware()->getCapability(FlightModes); i++) {
PhaseData *pd1=&g_model1->phaseData[i];
PhaseData *pd2=&g_model2->phaseData[i];
str.append("<tr><td><b>"+tr("FM")+QString("%1</b> ").arg(i));
color=getColor1(pd1->name,pd2->name);
str.append(QString("<font size=+1 face='Courier New' color=%2>%1</font></td>").arg(pd1->name).arg(color));
if (GetCurrentFirmware()->getCapability(GvarsFlightPhases)) {
if (GetCurrentFirmware()->getCapability(GvarsFlightModes)) {
for (k=0; k<gvarnum; k++) {
color=getColor1(pd1->gvars[k],pd2->gvars[k]);
if (pd1->gvars[k]<=1024) {
@ -411,7 +411,7 @@ void CompareDialog::printPhases()
str.append(QString("<td width=\"40\" align=\"center\"><b>%1</b></td>").arg(getInputStr(*g_model1, i)));
}
str.append("</tr>");
for (i=0; i<GetCurrentFirmware()->getCapability(FlightPhases); i++) {
for (i=0; i<GetCurrentFirmware()->getCapability(FlightModes); i++) {
PhaseData *pd1=&g_model1->phaseData[i];
PhaseData *pd2=&g_model2->phaseData[i];
str.append("<tr><td><b>"+tr("FM")+QString("%1</b> ").arg(i));
@ -436,17 +436,17 @@ void CompareDialog::printPhases()
}
str.append("</table>");
if ((gvars==1 && GetCurrentFirmware()->getCapability(GvarsFlightPhases)) || GetCurrentFirmware()->getCapability(RotaryEncoders)) {
if ((gvars==1 && GetCurrentFirmware()->getCapability(GvarsFlightModes)) || GetCurrentFirmware()->getCapability(RotaryEncoders)) {
str.append("<br><table border=1 cellspacing=0 cellpadding=1 width=\"100%\">");
str.append("<tr><td style=\"border-style:none;\">&nbsp;</td>");
if (GetCurrentFirmware()->getCapability(GvarsFlightPhases)) {
if (GetCurrentFirmware()->getCapability(GvarsFlightModes)) {
str.append(QString("<td colspan=%1 align=center><b>").arg(gvarnum)+tr("Gvars")+"</td>");
}
if (GetCurrentFirmware()->getCapability(RotaryEncoders)) {
str.append(QString("<td colspan=%1 align=center><b>").arg(GetCurrentFirmware()->getCapability(RotaryEncoders))+tr("Rot. Enc.")+"</td>");
}
str.append("</tr><tr><td align=center ><b>"+tr("Flight mode name")+"</b></td>");
if (GetCurrentFirmware()->getCapability(GvarsFlightPhases)) {
if (GetCurrentFirmware()->getCapability(GvarsFlightModes)) {
for (i=0; i<gvarnum; i++) {
str.append(QString("<td width=\"40\" align=\"center\"><b>GV%1</b><br>%2</td>").arg(i+1).arg(g_model2->gvars_names[i]));
}
@ -455,13 +455,13 @@ void CompareDialog::printPhases()
str.append(QString("<td align=\"center\"><b>RE%1</b></td>").arg((i==0 ? 'A': 'B')));
}
str.append("</tr>");
for (i=0; i<GetCurrentFirmware()->getCapability(FlightPhases); i++) {
for (i=0; i<GetCurrentFirmware()->getCapability(FlightModes); i++) {
PhaseData *pd1=&g_model1->phaseData[i];
PhaseData *pd2=&g_model2->phaseData[i];
str.append("<tr><td><b>"+tr("FM")+QString("%1</b> ").arg(i));
color=getColor1(pd1->name,pd2->name);
str.append(QString("<font size=+1 face='Courier New' color=%2>%1</font></td>").arg(pd2->name).arg(color));
if (GetCurrentFirmware()->getCapability(GvarsFlightPhases)) {
if (GetCurrentFirmware()->getCapability(GvarsFlightModes)) {
for (k=0; k<gvarnum; k++) {
color=getColor1(pd1->gvars[k],pd2->gvars[k]);
if (pd2->gvars[k]<=1024) {
@ -569,7 +569,7 @@ void CompareDialog::printGvars()
gvarnum=GetCurrentFirmware()->getCapability(Gvars);
}
if (!GetCurrentFirmware()->getCapability(GvarsFlightPhases) && (gvars==1 && GetCurrentFirmware()->getCapability(Gvars))) {
if (!GetCurrentFirmware()->getCapability(GvarsFlightModes) && (gvars==1 && GetCurrentFirmware()->getCapability(Gvars))) {
QString str = "<table border=1 cellspacing=0 cellpadding=3 width=\"100%\">";
str.append("<tr><td colspan=2><h2>"+tr("Global Variables")+"</h2></td></tr>");
str.append("<tr><td width=50%>");
@ -653,12 +653,12 @@ void CompareDialog::printExpos()
str += tr("Weight") + QString("%1").arg(getGVarString(ed->weight)).rightJustified(6, ' ');
str += ed->curve.toString().replace("<", "&lt;").replace(">", "&gt;");
if (GetCurrentFirmware()->getCapability(FlightPhases)) {
if (GetCurrentFirmware()->getCapability(FlightModes)) {
if(ed->phases) {
if (ed->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightPhases))-1) {
if (ed->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightModes))-1) {
int mask=1;
int first=0;
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightPhases);i++) {
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightModes);i++) {
if (!(ed->phases & mask)) {
first++;
}
@ -671,7 +671,7 @@ void CompareDialog::printExpos()
}
mask=1;
first=1;
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightPhases);j++) {
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightModes);j++) {
if (!(ed->phases & mask)) {
PhaseData *pd = &g_model1->phaseData[j];
if (!first) {
@ -731,12 +731,12 @@ void CompareDialog::printExpos()
str += tr("Weight") + QString("%1").arg(getGVarString(ed->weight)).rightJustified(6, ' ');
str += ed->curve.toString().replace("<", "&lt;").replace(">", "&gt;");
if (GetCurrentFirmware()->getCapability(FlightPhases)) {
if (GetCurrentFirmware()->getCapability(FlightModes)) {
if(ed->phases) {
if (ed->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightPhases))-1) {
if (ed->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightModes))-1) {
int mask=1;
int first=0;
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightPhases);i++) {
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightModes);i++) {
if (!(ed->phases & mask)) {
first++;
}
@ -749,7 +749,7 @@ void CompareDialog::printExpos()
}
mask=1;
first=1;
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightPhases);j++) {
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightModes);j++) {
if (!(ed->phases & mask)) {
PhaseData *pd = &g_model2->phaseData[j];
if (!first) {
@ -829,12 +829,12 @@ void CompareDialog::printMixers()
if (md->delayDown || md->delayUp) str += tr(" Delay(u%1:d%2)").arg(md->delayUp/scale).arg(md->delayDown/scale);
if (md->speedDown || md->speedUp) str += tr(" Slow(u%1:d%2)").arg(md->speedUp/scale).arg(md->speedDown/scale);
if (md->mixWarn) str += " "+tr("Warn")+QString("(%1)").arg(md->mixWarn);
if (GetCurrentFirmware()->getCapability(FlightPhases)) {
if (GetCurrentFirmware()->getCapability(FlightModes)) {
if(md->phases) {
if (md->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightPhases))-1) {
if (md->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightModes))-1) {
int mask=1;
int first=0;
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightPhases);i++) {
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightModes);i++) {
if (!(md->phases & mask)) {
first++;
}
@ -847,7 +847,7 @@ void CompareDialog::printMixers()
}
mask=1;
first=1;
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightPhases);j++) {
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightModes);j++) {
if (!(md->phases & mask)) {
PhaseData *pd = &g_model1->phaseData[j];
if (!first) {
@ -908,12 +908,12 @@ void CompareDialog::printMixers()
if (md->delayDown || md->delayUp) str += tr(" Delay(u%1:d%2)").arg(md->delayUp/scale).arg(md->delayDown/scale);
if (md->speedDown || md->speedUp) str += tr(" Slow(u%1:d%2)").arg(md->speedUp/scale).arg(md->speedDown/scale);
if (md->mixWarn) str += " "+tr("Warn")+QString("(%1)").arg(md->mixWarn);
if (GetCurrentFirmware()->getCapability(FlightPhases)) {
if (GetCurrentFirmware()->getCapability(FlightModes)) {
if(md->phases) {
if (md->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightPhases))-1) {
if (md->phases!=(unsigned int)(1<<GetCurrentFirmware()->getCapability(FlightModes))-1) {
int mask=1;
int first=0;
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightPhases);i++) {
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightModes);i++) {
if (!(md->phases & mask)) {
first++;
}
@ -926,7 +926,7 @@ void CompareDialog::printMixers()
}
mask=1;
first=1;
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightPhases);j++) {
for (int j=0; j<GetCurrentFirmware()->getCapability(FlightModes);j++) {
if (!(md->phases & mask)) {
PhaseData *pd = &g_model2->phaseData[j];
if (!first) {

24
companion/src/eeprominterface.cpp
View file

@ -200,8 +200,8 @@ RawSourceRange RawSource::getRange(bool singleprec)
result.decimals = 1;
break;
case TELEMETRY_SOURCE_CONSUMPTION:
result.step = singleprec ? 20 : 1;
result.max = singleprec ? 5100 : 10000;
result.step = singleprec ? 100 : 1;
result.max = singleprec ? 25500 : 10000;
break;
case TELEMETRY_SOURCE_POWER:
case TELEMETRY_SOURCE_POWER_MAX:
@ -272,7 +272,7 @@ QString RawSource::toString()
QObject::tr("ACC"), QObject::tr("Time"),
};
static const QString virtualSwitches[] = {
static const QString logicalSwitches[] = {
QObject::tr("L1"), QObject::tr("L2"), QObject::tr("L3"), QObject::tr("L4"), QObject::tr("L5"), QObject::tr("L6"), QObject::tr("L7"), QObject::tr("L8"), QObject::tr("L9"), QObject::tr("L10"),
QObject::tr("L11"), QObject::tr("L12"), QObject::tr("L13"), QObject::tr("L14"), QObject::tr("L15"), QObject::tr("L16"), QObject::tr("L17"), QObject::tr("L18"), QObject::tr("L19"), QObject::tr("L20"),
QObject::tr("L21"), QObject::tr("L22"), QObject::tr("L23"), QObject::tr("L24"), QObject::tr("L25"), QObject::tr("L26"), QObject::tr("L27"), QObject::tr("L28"), QObject::tr("L29"), QObject::tr("L30"),
@ -302,7 +302,7 @@ QString RawSource::toString()
case SOURCE_TYPE_SWITCH:
return (IS_TARANIS(GetEepromInterface()->getBoard()) ? CHECK_IN_ARRAY(switchesX9D, index) : CHECK_IN_ARRAY(switches9X, index));
case SOURCE_TYPE_CUSTOM_SWITCH:
return virtualSwitches[index];
return logicalSwitches[index];
case SOURCE_TYPE_CYC:
return QObject::tr("CYC%1").arg(index+1);
case SOURCE_TYPE_PPM:
@ -349,13 +349,17 @@ QString RawSwitch::toString()
SwitchUp('H'), SwitchDn('H'),
};
static const QString virtualSwitches[] = {
static const QString logicalSwitches[] = {
QObject::tr("L1"), QObject::tr("L2"), QObject::tr("L3"), QObject::tr("L4"), QObject::tr("L5"), QObject::tr("L6"), QObject::tr("L7"), QObject::tr("L8"), QObject::tr("L9"), QObject::tr("L10"),
QObject::tr("L11"), QObject::tr("L12"), QObject::tr("L13"), QObject::tr("L14"), QObject::tr("L15"), QObject::tr("L16"), QObject::tr("L17"), QObject::tr("L18"), QObject::tr("L19"), QObject::tr("L20"),
QObject::tr("L21"), QObject::tr("L22"), QObject::tr("L23"), QObject::tr("L24"), QObject::tr("L25"), QObject::tr("L26"), QObject::tr("L27"), QObject::tr("L28"), QObject::tr("L29"), QObject::tr("L30"),
QObject::tr("L31"), QObject::tr("L32")
};
static const QString flightModes[] = {
QObject::tr("FM0"), QObject::tr("FM1"), QObject::tr("FM2"), QObject::tr("FM3"), QObject::tr("FM4"), QObject::tr("FM5"), QObject::tr("FM6"), QObject::tr("FM7"), QObject::tr("FM8")
};
static const QString multiposPots[] = {
QObject::tr("S11"), QObject::tr("S12"), QObject::tr("S13"), QObject::tr("S14"), QObject::tr("S15"), QObject::tr("S16"),
QObject::tr("S21"), QObject::tr("S22"), QObject::tr("S23"), QObject::tr("S24"), QObject::tr("S25"), QObject::tr("S26"),
@ -389,7 +393,7 @@ QString RawSwitch::toString()
else
return CHECK_IN_ARRAY(switches9X, index-1);
case SWITCH_TYPE_VIRTUAL:
return CHECK_IN_ARRAY(virtualSwitches, index-1);
return CHECK_IN_ARRAY(logicalSwitches, index-1);
case SWITCH_TYPE_MULTIPOS_POT:
return CHECK_IN_ARRAY(multiposPots, index-1);
case SWITCH_TYPE_TRIM:
@ -400,6 +404,8 @@ QString RawSwitch::toString()
return QObject::tr("ON");
case SWITCH_TYPE_OFF:
return QObject::tr("OFF");
case SWITCH_TYPE_FLIGHT_MODE:
return CHECK_IN_ARRAY(flightModes, index-1);
case SWITCH_TYPE_NONE:
return QObject::tr("----");
case SWITCH_TYPE_TIMER_MODE:
@ -1060,7 +1066,7 @@ void ModelData::clear()
moduleData[0].protocol=PPM;
moduleData[1].protocol=OFF;
}
for (int i=0; i<C9X_MAX_PHASES; i++)
for (int i=0; i<C9X_MAX_FLIGHT_MODES; i++)
phaseData[i].clear();
clearInputs();
clearMixes();
@ -1130,7 +1136,7 @@ void ModelData::setDefaultValues(unsigned int id, const GeneralSettings & settin
int ModelData::getTrimValue(int phaseIdx, int trimIdx)
{
int result = 0;
for (int i=0; i<C9X_MAX_PHASES; i++) {
for (int i=0; i<C9X_MAX_FLIGHT_MODES; i++) {
PhaseData & phase = phaseData[phaseIdx];
if (phase.trimMode[trimIdx] < 0) {
return result;
@ -1153,7 +1159,7 @@ int ModelData::getTrimValue(int phaseIdx, int trimIdx)
void ModelData::setTrimValue(int phaseIdx, int trimIdx, int value)
{
for (uint8_t i=0; i<C9X_MAX_PHASES; i++) {
for (uint8_t i=0; i<C9X_MAX_FLIGHT_MODES; i++) {
PhaseData & phase = phaseData[phaseIdx];
int mode = phase.trimMode[trimIdx];
int p = phase.trimRef[trimIdx];

13
companion/src/eeprominterface.h
View file

@ -64,7 +64,7 @@ const uint8_t modn12x3[4][4]= {
{4, 3, 2, 1} };
#define C9X_MAX_MODELS 60
#define C9X_MAX_PHASES 9
#define C9X_MAX_FLIGHT_MODES 9
#define C9X_MAX_MIXERS 64
#define C9X_MAX_INPUTS 32
#define C9X_MAX_EXPOS 64
@ -369,6 +369,7 @@ enum RawSwitchType {
SWITCH_TYPE_ROTARY_ENCODER,
SWITCH_TYPE_ON,
SWITCH_TYPE_OFF,
SWITCH_TYPE_FLIGHT_MODE,
SWITCH_TYPE_TIMER_MODE
};
@ -955,7 +956,7 @@ class ModelData {
bool extendedLimits; // TODO xml
bool extendedTrims;
bool throttleReversed;
PhaseData phaseData[C9X_MAX_PHASES];
PhaseData phaseData[C9X_MAX_FLIGHT_MODES];
MixData mixData[C9X_MAX_MIXERS];
LimitData limitData[C9X_NUM_CHNOUT];
@ -1019,9 +1020,9 @@ class RadioData {
// TODO rename FlightPhase to FlightMode
enum Capability {
FlightPhases,
FlightModes,
FlightModesName,
FlightPhasesHaveFades,
FlightModesHaveFades,
Mixes,
MixesWithoutExpo,
Timers,
@ -1077,7 +1078,7 @@ enum Capability {
Gvars,
GvarsInCS,
GvarsAreNamed,
GvarsFlightPhases,
GvarsFlightModes,
GvarsName,
NoTelemetryProtocol,
TelemetryCustomScreens,
@ -1199,7 +1200,7 @@ inline void applyStickModeToModel(ModelData &model, unsigned int mode)
ModelData model_copy = model;
// trims
for (int p=0; p<C9X_MAX_PHASES; p++) {
for (int p=0; p<C9X_MAX_FLIGHT_MODES; p++) {
for (int i=0; i<NUM_STICKS/2; i++) {
int converted_stick = applyStickMode(i+1, mode) - 1;
int tmp = model.phaseData[p].trim[i];

8
companion/src/firmwares/gruvin9x/gruvin9xeeprom.cpp
View file

@ -455,7 +455,7 @@ t_Gruvin9xModelData_v102::operator ModelData ()
c9x.beepANACenter = beepANACenter;
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
for (int i=0; i<G9X_MAX_PHASES; i++)
for (int i=0; i<G9X_MAX_FLIGHT_MODES; i++)
c9x.phaseData[i] = phaseData[i];
for (int i=0; i<G9X_MAX_MIXERS; i++)
c9x.mixData[i] = mixData[i];
@ -526,7 +526,7 @@ t_Gruvin9xModelData_v103::operator ModelData ()
c9x.beepANACenter = beepANACenter;
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
for (int i=0; i<G9X_MAX_PHASES; i++)
for (int i=0; i<G9X_MAX_FLIGHT_MODES; i++)
c9x.phaseData[i] = phaseData[i];
for (int i=0; i<G9X_MAX_MIXERS; i++)
c9x.mixData[i] = mixData[i];
@ -598,7 +598,7 @@ t_Gruvin9xModelData_v105::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<G9X_MAX_PHASES; i++) {
for (int i=0; i<G9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (phaseData[i].trim[j] > 125) {
@ -689,7 +689,7 @@ t_Gruvin9xModelData_v106::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<G9X_MAX_PHASES; i++) {
for (int i=0; i<G9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {

10
companion/src/firmwares/gruvin9x/gruvin9xeeprom.h
View file

@ -277,7 +277,7 @@ PACK(typedef struct t_Gruvin9xTimerData {
t_Gruvin9xTimerData() { memset(this, 0, sizeof(t_Gruvin9xTimerData)); }
}) Gruvin9xTimerData;
#define G9X_MAX_PHASES 5
#define G9X_MAX_FLIGHT_MODES 5
#define G9X_MAX_MIXERS 32
#define G9X_MAX_EXPOS 14
#define G9X_MAX_CURVE5 8
@ -312,7 +312,7 @@ PACK(typedef struct t_Gruvin9xModelData_v102 {
Gruvin9xLogicalSwitchData customSw[G9X_NUM_CSW];
Gruvin9xSafetySwData safetySw[G9X_NUM_CHNOUT];
Gruvin9xSwashRingData swashR;
Gruvin9xPhaseData_v102 phaseData[G9X_MAX_PHASES];
Gruvin9xPhaseData_v102 phaseData[G9X_MAX_FLIGHT_MODES];
Gruvin9xFrSkyData frsky;
operator ModelData();
@ -344,7 +344,7 @@ PACK(typedef struct t_Gruvin9xModelData_v103 {
Gruvin9xLogicalSwitchData customSw[G9X_NUM_CSW];
Gruvin9xSafetySwData safetySw[G9X_NUM_CHNOUT];
Gruvin9xSwashRingData swashR;
Gruvin9xPhaseData_v102 phaseData[G9X_MAX_PHASES];
Gruvin9xPhaseData_v102 phaseData[G9X_MAX_FLIGHT_MODES];
Gruvin9xFrSkyData frsky;
operator ModelData();
@ -377,7 +377,7 @@ PACK(typedef struct t_Gruvin9xModelData_v105 {
Gruvin9xSafetySwData safetySw[G9X_NUM_CHNOUT];
Gruvin9xFuncSwData funcSw[G9X_NUM_FSW];
Gruvin9xSwashRingData swashR;
Gruvin9xPhaseData_v102 phaseData[G9X_MAX_PHASES];
Gruvin9xPhaseData_v102 phaseData[G9X_MAX_FLIGHT_MODES];
int16_t subtrim[NUM_STICKS];
Gruvin9xFrSkyData frsky;
@ -409,7 +409,7 @@ PACK(typedef struct t_Gruvin9xModelData_v106 {
Gruvin9xSafetySwData safetySw[G9X_NUM_CHNOUT];
Gruvin9xFuncSwData funcSw[G9X_NUM_FSW];
Gruvin9xSwashRingData swashR;
Gruvin9xPhaseData_v106 phaseData[G9X_MAX_PHASES];
Gruvin9xPhaseData_v106 phaseData[G9X_MAX_FLIGHT_MODES];
Gruvin9xFrSkyData frsky;
operator ModelData();

10
companion/src/firmwares/opentx/open9xGruvin9xeeprom.cpp
View file

@ -460,7 +460,7 @@ t_Open9xGruvin9xModelData_v207::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -545,7 +545,7 @@ t_Open9xGruvin9xModelData_v208::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -634,7 +634,7 @@ t_Open9xGruvin9xModelData_v209::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -724,7 +724,7 @@ t_Open9xGruvin9xModelData_v210::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -811,7 +811,7 @@ t_Open9xGruvin9xModelData_v211::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {

10
companion/src/firmwares/opentx/open9xGruvin9xeeprom.h
View file

@ -197,7 +197,7 @@ PACK(typedef struct t_Open9xGruvin9xModelData_v207 {
Open9xGruvin9xLogicalSwitchData_v207 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xGruvin9xSwashRingData_v208 swashR;
Open9xGruvin9xPhaseData_v207 phaseData[O9X_MAX_PHASES];
Open9xGruvin9xPhaseData_v207 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v205 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -231,7 +231,7 @@ PACK(typedef struct t_Open9xGruvin9xModelData_v208 {
Open9xGruvin9xLogicalSwitchData_v207 customSw[O9X_NUM_CSW];
Open9xGruvin9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xGruvin9xSwashRingData_v208 swashR;
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_PHASES];
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v208 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -270,7 +270,7 @@ PACK(typedef struct t_Open9xGruvin9xModelData_v209 {
Open9xGruvin9xLogicalSwitchData_v209 customSw[O9X_NUM_CSW];
Open9xGruvin9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xGruvin9xSwashRingData_v209 swashR;
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_PHASES];
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v208 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -310,7 +310,7 @@ PACK(typedef struct t_Open9xGruvin9xModelData_v210 {
Open9xGruvin9xLogicalSwitchData_v209 customSw[O9X_NUM_CSW];
Open9xGruvin9xFuncSwData_v210 funcSw[O9X_NUM_FSW];
Open9xGruvin9xSwashRingData_v209 swashR;
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_PHASES];
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -348,7 +348,7 @@ PACK(typedef struct t_Open9xGruvin9xModelData_v211 {
Open9xGruvin9xLogicalSwitchData_v209 customSw[O9X_NUM_CSW];
Open9xGruvin9xFuncSwData_v210 funcSw[O9X_NUM_FSW];
Open9xGruvin9xSwashRingData_v209 swashR;
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_PHASES];
Open9xGruvin9xPhaseData_v208 phaseData[O9X_MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;

10
companion/src/firmwares/opentx/open9xSky9xeeprom.cpp
View file

@ -767,7 +767,7 @@ t_Open9xArmModelData_v208::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_ARM_MAX_PHASES; i++) {
for (int i=0; i<O9X_ARM_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -856,7 +856,7 @@ t_Open9xArmModelData_v209::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_ARM_MAX_PHASES; i++) {
for (int i=0; i<O9X_ARM_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -946,7 +946,7 @@ t_Open9xArmModelData_v210::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_ARM_MAX_PHASES; i++) {
for (int i=0; i<O9X_ARM_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1030,7 +1030,7 @@ t_Open9xArmModelData_v211::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_ARM_MAX_PHASES; i++) {
for (int i=0; i<O9X_ARM_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1117,7 +1117,7 @@ t_Open9xArmModelData_v212::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_ARM_MAX_PHASES; i++) {
for (int i=0; i<O9X_ARM_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {

12
companion/src/firmwares/opentx/open9xSky9xeeprom.h
View file

@ -19,7 +19,7 @@
#include "open9xStockeeprom.h"
#define O9X_ARM_MAX_PHASES 9
#define O9X_ARM_MAX_FLIGHT_MODES 9
#define O9X_ARM_MAX_MIXERS 64
#define O9X_ARM_MAX_EXPOS 32
#define O9X_ARM_NUM_CHNOUT 32 // number of real output channels CH1-CH16
@ -346,7 +346,7 @@ PACK(typedef struct t_Open9xArmModelData_v208 {
Open9xArmLogicalSwitchData_v208 customSw[O9X_ARM_NUM_CSW];
Open9xArmFuncSwData_v208 funcSw[O9X_ARM_NUM_FSW];
Open9xArmSwashRingData_v208 swashR;
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_PHASES];
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_FLIGHT_MODES];
Open9xFrSkyData_v208 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -385,7 +385,7 @@ PACK(typedef struct t_Open9xArmModelData_v209 {
Open9xArmLogicalSwitchData_v209 customSw[O9X_ARM_NUM_CSW];
Open9xArmFuncSwData_v208 funcSw[O9X_ARM_NUM_FSW];
Open9xArmSwashRingData_v209 swashR;
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_PHASES];
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_FLIGHT_MODES];
Open9xFrSkyData_v208 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -425,7 +425,7 @@ PACK(typedef struct t_Open9xArmModelData_v210 {
Open9xArmLogicalSwitchData_v210 customSw[O9X_ARM_NUM_CSW];
Open9xArmFuncSwData_v210 funcSw[O9X_ARM_NUM_FSW];
Open9xArmSwashRingData_v209 swashR;
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_PHASES];
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_FLIGHT_MODES];
Open9xArmFrSkyData_v210 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -464,7 +464,7 @@ PACK(typedef struct t_Open9xArmModelData_v211 {
Open9xArmLogicalSwitchData_v210 customSw[O9X_ARM_NUM_CSW];
Open9xArmFuncSwData_v211 funcSw[O9X_ARM_NUM_FSW];
Open9xArmSwashRingData_v209 swashR;
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_PHASES];
Open9xArmPhaseData_v208 phaseData[O9X_ARM_MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -502,7 +502,7 @@ PACK(typedef struct t_Open9xArmModelData_v212 {
Open9xArmLogicalSwitchData_v210 customSw[O9X_ARM_NUM_CSW];
Open9xArmFuncSwData_v211 funcSw[O9X_ARM_NUM_FSW];
Open9xArmSwashRingData_v210 swashR;
Open9xArmPhaseData_v212 phaseData[O9X_ARM_MAX_PHASES];
Open9xArmPhaseData_v212 phaseData[O9X_ARM_MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;

18
companion/src/firmwares/opentx/open9xStockeeprom.cpp
View file

@ -948,7 +948,7 @@ t_Open9xModelData_v201::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1022,7 +1022,7 @@ t_Open9xModelData_v202::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1098,7 +1098,7 @@ t_Open9xModelData_v203::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1172,7 +1172,7 @@ t_Open9xModelData_v204::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1251,7 +1251,7 @@ t_Open9xModelData_v205::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1337,7 +1337,7 @@ t_Open9xModelData_v208::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1430,7 +1430,7 @@ t_Open9xModelData_v209::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1524,7 +1524,7 @@ t_Open9xModelData_v210::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {
@ -1612,7 +1612,7 @@ t_Open9xModelData_v211::operator ModelData ()
c9x.moduleData[0].ppmPulsePol = pulsePol;
c9x.extendedLimits = extendedLimits;
c9x.extendedTrims = extendedTrims;
for (int i=0; i<O9X_MAX_PHASES; i++) {
for (int i=0; i<O9X_MAX_FLIGHT_MODES; i++) {
c9x.phaseData[i] = phaseData[i];
for (int j=0; j<NUM_STICKS; j++) {
if (c9x.phaseData[i].trim[j] > 500) {

20
companion/src/firmwares/opentx/open9xStockeeprom.h
View file

@ -482,7 +482,7 @@ PACK(typedef struct t_Open9xTimerDataExtra {
}) Open9xTimerDataExtra;
#define O9X_MAX_TIMERS 2
#define O9X_MAX_PHASES 5
#define O9X_MAX_FLIGHT_MODES 5
#define O9X_MAX_MIXERS 32
#define O9X_MAX_EXPOS 14
#define O9X_NUM_CHNOUT 16 // number of real output channels CH1-CH16
@ -520,7 +520,7 @@ PACK(typedef struct t_Open9xModelData_v201 {
Open9xSafetySwData safetySw[O9X_NUM_CHNOUT];
Open9xFuncSwData_v201 funcSw[12];
Open9xSwashRingData_v208 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v201 frsky;
operator ModelData();
@ -551,7 +551,7 @@ PACK(typedef struct t_Open9xModelData_v202 {
Open9xSafetySwData safetySw[O9X_NUM_CHNOUT];
Open9xFuncSwData_v201 funcSw[12];
Open9xSwashRingData_v208 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v202 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -584,7 +584,7 @@ PACK(typedef struct t_Open9xModelData_v203 {
Open9xLogicalSwitchData_v208 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v208 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v202 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -617,7 +617,7 @@ PACK(typedef struct t_Open9xModelData_v204 {
Open9xLogicalSwitchData_v208 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v208 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v204 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -650,7 +650,7 @@ PACK(typedef struct t_Open9xModelData_v205 {
Open9xLogicalSwitchData_v208 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v208 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v205 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -685,7 +685,7 @@ PACK(typedef struct t_Open9xModelData_v208 {
Open9xLogicalSwitchData_v208 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v208 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v208 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -724,7 +724,7 @@ PACK(typedef struct t_Open9xModelData_v209 {
Open9xLogicalSwitchData_v209 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v203 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v209 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
Open9xFrSkyData_v208 frsky;
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -764,7 +764,7 @@ PACK(typedef struct t_Open9xModelData_v210 {
Open9xLogicalSwitchData_v209 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v210 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v209 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;
@ -802,7 +802,7 @@ PACK(typedef struct t_Open9xModelData_v211 {
Open9xLogicalSwitchData_v209 customSw[O9X_NUM_CSW];
Open9xFuncSwData_v210 funcSw[O9X_NUM_FSW];
Open9xSwashRingData_v209 swashR;
Open9xPhaseData_v201 phaseData[O9X_MAX_PHASES];
Open9xPhaseData_v201 phaseData[O9X_MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5msec increments
uint8_t thrTraceSrc;

11
companion/src/firmwares/opentx/opentxeeprom.cpp
View file

@ -15,7 +15,7 @@
#define MAX_SWITCHES(board) (IS_TARANIS(board) ? 8 : 7)
#define MAX_SWITCHES_POSITION(board) (IS_TARANIS(board) ? 22 : 9)
#define MAX_ROTARY_ENCODERS(board) (board==BOARD_GRUVIN9X ? 2 : (board==BOARD_SKY9X ? 1 : 0))
#define MAX_PHASES(board, version) (IS_ARM(board) ? 9 : (IS_DBLRAM(board, version) ? 6 : 5))
#define MAX_FLIGHT_MODES(board, version) (IS_ARM(board) ? 9 : (IS_DBLRAM(board, version) ? 6 : 5))
#define MAX_MIXERS(board, version) (IS_ARM(board) ? 64 : 32)
#define MAX_CHANNELS(board, version) (IS_ARM(board) ? 32 : 16)
#define MAX_EXPOS(board, version) (IS_ARM(board) ? ((IS_TARANIS(board) && version >= 216) ? 64 : 32) : (IS_DBLRAM(board, version) ? 16 : 14))
@ -91,6 +91,13 @@ class SwitchesConversionTable: public ConversionTable {
addConversion(RawSwitch(SWITCH_TYPE_ON), val++);
}
if (IS_ARM(board)) {
for (int i=1; i<=MAX_FLIGHT_MODES(board, version); i++) {
addConversion(RawSwitch(SWITCH_TYPE_FLIGHT_MODE, -i), -val+offset);
addConversion(RawSwitch(SWITCH_TYPE_FLIGHT_MODE, i), val++);
}
}
if (version < 216) {
// previous "moment" switches
for (int i=1; i<=MAX_SWITCHES_POSITION(board); i++) {
@ -2401,7 +2408,7 @@ OpenTxModelData::OpenTxModelData(ModelData & modelData, BoardEnum board, unsigne
internalField.Append(new AvrCustomFunctionField(modelData.funcSw[i], board, version, variant));
}
internalField.Append(new HeliField(modelData.swashRingData, board, version, variant));
for (int i=0; i<MAX_PHASES(board, version); i++)
for (int i=0; i<MAX_FLIGHT_MODES(board, version); i++)
internalField.Append(new FlightModeField(modelData.phaseData[i], i, board, version));
if (!IS_ARM(board) || version < 216) {

4
companion/src/firmwares/opentx/opentxeeprom.h
View file

@ -32,7 +32,7 @@
#define SIMU_M128_VARIANTS (M128_VARIANT|SIMU_STOCK_VARIANTS)
#define O9X_MAX_TIMERS 2
#define O9X_MAX_PHASES 5
#define O9X_MAX_FLIGHT_MODES 5
#define O9X_MAX_MIXERS 32
#define O9X_MAX_EXPOS 14
#define O9X_NUM_CHNOUT 16 // number of real output channels CH1-CH16
@ -41,7 +41,7 @@
#define O9X_MAX_CURVES 8
#define O9X_NUM_POINTS (112-O9X_MAX_CURVES)
#define O9X_ARM_MAX_PHASES 9
#define O9X_ARM_MAX_FLIGHT_MODES 9
#define O9X_ARM_MAX_MIXERS 64
#define O9X_ARM_MAX_EXPOS 32
#define O9X_ARM_NUM_CHNOUT 32 // number of real output channels CH1-CH16

8
companion/src/firmwares/opentx/opentxinterface.cpp
View file

@ -478,14 +478,14 @@ int OpenTxFirmware::getCapability(const Capability capability)
return 1;
case PPMFrameLength:
return 40;
case FlightPhases:
case FlightModes:
if (IS_ARM(board))
return 9;
else if (board==BOARD_GRUVIN9X)
return 6;
else
return 5;
case FlightPhasesHaveFades:
case FlightModesHaveFades:
return 1;
case Gvars:
return IS_ARM(board) ? 9 : 5;
@ -499,7 +499,7 @@ int OpenTxFirmware::getCapability(const Capability capability)
case HasFAIMode:
return 1;
case GvarsAreNamed:
case GvarsFlightPhases:
case GvarsFlightModes:
return ((IS_ARM(board)||(board==BOARD_GRUVIN9X)) ? 1 : 0);
case Mixes:
return (IS_ARM(board) ? O9X_ARM_MAX_MIXERS : O9X_MAX_MIXERS);
@ -802,7 +802,7 @@ bool OpenTxEepromInterface::checkVersion(unsigned int version)
break;
// case 206:
case 207:
// V4: Rotary Encoders position in FlightPhases
// V4: Rotary Encoders position in FlightModes
break;
case 208:
// Trim value in 16bits

22
companion/src/helpers.cpp
View file

@ -129,7 +129,7 @@ QString getProtocolStr(const int proto)
void populatePhasesCB(QComboBox *b, int value)
{
for (int i=-GetCurrentFirmware()->getCapability(FlightPhases); i<=GetCurrentFirmware()->getCapability(FlightPhases); i++) {
for (int i=-GetCurrentFirmware()->getCapability(FlightModes); i<=GetCurrentFirmware()->getCapability(FlightModes); i++) {
if (i < 0)
b->addItem(QObject::tr("!Flight mode %1").arg(-i-1), i);
else if (i > 0)
@ -137,7 +137,7 @@ void populatePhasesCB(QComboBox *b, int value)
else
b->addItem(QObject::tr("----"), 0);
}
b->setCurrentIndex(value + GetCurrentFirmware()->getCapability(FlightPhases));
b->setCurrentIndex(value + GetCurrentFirmware()->getCapability(FlightModes));
}
bool gvarsEnabled()
@ -344,7 +344,7 @@ void CurveGroup::valuesChanged()
void populateGvarUseCB(QComboBox *b, unsigned int phase)
{
b->addItem(QObject::tr("Own value"));
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightPhases); i++) {
for (int i=0; i<GetCurrentFirmware()->getCapability(FlightModes); i++) {
if (i != (int)phase) {
b->addItem(QObject::tr("Flight mode %1 value").arg(i));
}
@ -400,6 +400,13 @@ void populateSwitchCB(QComboBox *b, const RawSwitch & value, const GeneralSettin
b->clear();
if (attr & POPULATE_ONOFF) {
if (IS_ARM(GetCurrentFirmware()->getBoard())) {
for (int i=-GetCurrentFirmware()->getCapability(FlightModes); i<0; i++) {
item = RawSwitch(SWITCH_TYPE_FLIGHT_MODE, i);
b->addItem(item.toString(), item.toValue());
if (item == value) b->setCurrentIndex(b->count()-1);
}
}
item = RawSwitch(SWITCH_TYPE_OFF);
b->addItem(item.toString(), item.toValue());
if (item == value) b->setCurrentIndex(b->count()-1);
@ -490,6 +497,13 @@ void populateSwitchCB(QComboBox *b, const RawSwitch & value, const GeneralSettin
item = RawSwitch(SWITCH_TYPE_ON);
b->addItem(item.toString(), item.toValue());
if (item == value) b->setCurrentIndex(b->count()-1);
if (IS_ARM(GetCurrentFirmware()->getBoard())) {
for (int i=1; i<=GetCurrentFirmware()->getCapability(FlightModes); i++) {
item = RawSwitch(SWITCH_TYPE_FLIGHT_MODE, i);
b->addItem(item.toString(), item.toValue());
if (item == value) b->setCurrentIndex(b->count()-1);
}
}
}
b->setMaxVisibleItems(10);
@ -835,7 +849,7 @@ QString getProtocol(ModelData * g_model)
QString getPhasesStr(unsigned int phases, ModelData & model)
{
int numphases = GetCurrentFirmware()->getCapability(FlightPhases);
int numphases = GetCurrentFirmware()->getCapability(FlightModes);
if (numphases && phases) {
QString str;

6
companion/src/modeledit/customfunctions.cpp
View file

@ -329,8 +329,14 @@ void CustomFunctionsPanel::refreshCustomFunction(int i, bool modified)
if (modified) model.funcSw[i].param = fswtchParam[i]->value();
fswtchParam[i]->setDecimals(0);
fswtchParam[i]->setSingleStep(1);
if (IS_ARM(GetEepromInterface()->getBoard())) {
fswtchParam[i]->setMinimum(-500);
fswtchParam[i]->setMaximum(500);
}
else {
fswtchParam[i]->setMinimum(-125);
fswtchParam[i]->setMaximum(125);
}
fswtchParam[i]->setValue(model.funcSw[i].param);
widgetsMask |= CUSTOM_FUNCTION_NUMERIC_PARAM;
}

12
companion/src/modeledit/expodialog.cpp
View file

@ -29,7 +29,7 @@ ExpoDialog::ExpoDialog(QWidget *parent, ModelData & model, ExpoData *expoData, G
ui->sideCB->setCurrentIndex(ed->mode-1);
if (!firmware->getCapability(FlightPhases)) {
if (!firmware->getCapability(FlightModes)) {
ui->label_phases->hide();
for (int i=0; i<9; i++) {
lb_fp[i]->hide();
@ -44,7 +44,7 @@ ExpoDialog::ExpoDialog(QWidget *parent, ModelData & model, ExpoData *expoData, G
}
mask <<= 1;
}
for (int i=firmware->getCapability(FlightPhases); i<9;i++) {
for (int i=firmware->getCapability(FlightModes); i<9;i++) {
lb_fp[i]->hide();
cb_fp[i]->hide();
}
@ -154,11 +154,11 @@ void ExpoDialog::valuesChanged()
ed->phases<<=1;
}
ed->phases>>=1;
if (firmware->getCapability(FlightPhases)) {
if (firmware->getCapability(FlightModes)) {
int zeros=0;
int ones=0;
int phtemp=ed->phases;
for (int i=0; i<firmware->getCapability(FlightPhases); i++) {
for (int i=0; i<firmware->getCapability(FlightModes); i++) {
if (phtemp & 1) {
ones++;
}
@ -169,7 +169,7 @@ void ExpoDialog::valuesChanged()
}
if (zeros==1) {
phtemp=ed->phases;
for (int i=0; i<firmware->getCapability(FlightPhases); i++) {
for (int i=0; i<firmware->getCapability(FlightModes); i++) {
if ((phtemp & 1)==0) {
break;
}
@ -178,7 +178,7 @@ void ExpoDialog::valuesChanged()
}
else if (ones==1) {
phtemp=ed->phases;
for (int i=0; i<firmware->getCapability(FlightPhases); i++) {
for (int i=0; i<firmware->getCapability(FlightModes); i++) {
if (phtemp & 1) {
break;
}

58
companion/src/modeledit/flightmodes.cpp
View file

@ -5,7 +5,7 @@
#include <QComboBox>
#include <QGridLayout>
FlightMode::FlightMode(QWidget * parent, ModelData & model, int phaseIdx, GeneralSettings & generalSettings, FirmwareInterface * firmware):
FlightModePanel::FlightModePanel(QWidget * parent, ModelData & model, int phaseIdx, GeneralSettings & generalSettings, FirmwareInterface * firmware):
ModelPanel(parent, model, generalSettings, firmware),
ui(new Ui::FlightMode),
phaseIdx(phaseIdx),
@ -16,7 +16,7 @@ FlightMode::FlightMode(QWidget * parent, ModelData & model, int phaseIdx, Genera
{
ui->setupUi(this);
int modesCount = firmware->getCapability(FlightPhases);
int modesCount = firmware->getCapability(FlightModes);
// Phase name
QRegExp rx(CHAR_FOR_NAMES_REGEX);
@ -39,7 +39,7 @@ FlightMode::FlightMode(QWidget * parent, ModelData & model, int phaseIdx, Genera
}
// FadeIn / FadeOut
if (firmware->getCapability(FlightPhasesHaveFades)) {
if (firmware->getCapability(FlightModesHaveFades)) {
int scale = firmware->getCapability(SlowScale);
int range = firmware->getCapability(SlowRange);
ui->fadeIn->setMaximum(float(range)/scale);
@ -174,12 +174,12 @@ FlightMode::FlightMode(QWidget * parent, ModelData & model, int phaseIdx, Genera
update();
}
FlightMode::~FlightMode()
FlightModePanel::~FlightModePanel()
{
delete ui;
}
void FlightMode::update()
void FlightModePanel::update()
{
ui->name->setText(phase.name);
@ -232,7 +232,7 @@ void FlightMode::update()
}
}
void FlightMode::phaseName_editingFinished()
void FlightModePanel::phaseName_editingFinished()
{
QLineEdit *lineEdit = qobject_cast<QLineEdit*>(sender());
strcpy(phase.name, lineEdit->text().toAscii());
@ -240,14 +240,14 @@ void FlightMode::phaseName_editingFinished()
emit nameModified();
}
void FlightMode::phaseSwitch_currentIndexChanged(int index)
void FlightModePanel::phaseSwitch_currentIndexChanged(int index)
{
QComboBox *comboBox = qobject_cast<QComboBox*>(sender());
phase.swtch = RawSwitch(comboBox->itemData(index).toInt());
emit modified();
}
void FlightMode::phaseFadeIn_editingFinished()
void FlightModePanel::phaseFadeIn_editingFinished()
{
QDoubleSpinBox *spinBox = qobject_cast<QDoubleSpinBox*>(sender());
int scale = firmware->getCapability(SlowScale);
@ -255,7 +255,7 @@ void FlightMode::phaseFadeIn_editingFinished()
emit modified();
}
void FlightMode::phaseFadeOut_editingFinished()
void FlightModePanel::phaseFadeOut_editingFinished()
{
QDoubleSpinBox *spinBox = qobject_cast<QDoubleSpinBox*>(sender());
int scale = firmware->getCapability(SlowScale);
@ -263,7 +263,7 @@ void FlightMode::phaseFadeOut_editingFinished()
emit modified();
}
void FlightMode::trimUpdate(unsigned int trim)
void FlightModePanel::trimUpdate(unsigned int trim)
{
lock = true;
int chn = CONVERT_MODE(trim+1)-1;
@ -283,7 +283,7 @@ void FlightMode::trimUpdate(unsigned int trim)
lock = false;
}
void FlightMode::phaseGVValue_editingFinished()
void FlightModePanel::phaseGVValue_editingFinished()
{
if (!lock) {
QSpinBox *spinBox = qobject_cast<QSpinBox*>(sender());
@ -293,7 +293,7 @@ void FlightMode::phaseGVValue_editingFinished()
}
}
void FlightMode::GVName_editingFinished()
void FlightModePanel::GVName_editingFinished()
{
if (!lock) {
QLineEdit *lineedit = qobject_cast<QLineEdit*>(sender());
@ -304,7 +304,7 @@ void FlightMode::GVName_editingFinished()
}
}
void FlightMode::GVSource_currentIndexChanged(int index)
void FlightModePanel::GVSource_currentIndexChanged(int index)
{
QComboBox *comboBox = qobject_cast<QComboBox*>(sender());
int gvar = comboBox->property("index").toInt();
@ -312,7 +312,7 @@ void FlightMode::GVSource_currentIndexChanged(int index)
emit modified();
}
void FlightMode::phaseGVUse_currentIndexChanged(int index)
void FlightModePanel::phaseGVUse_currentIndexChanged(int index)
{
if (!lock) {
lock = true;
@ -330,14 +330,14 @@ void FlightMode::phaseGVUse_currentIndexChanged(int index)
}
}
void FlightMode::phaseGVPopupToggled(bool checked)
void FlightModePanel::phaseGVPopupToggled(bool checked)
{
QCheckBox *cb = qobject_cast<QCheckBox*>(sender());
int gvar = cb->property("index").toInt();
model.gvars_popups[gvar] = checked;
}
void FlightMode::phaseREValue_editingFinished()
void FlightModePanel::phaseREValue_editingFinished()
{
if (!lock) {
QSpinBox *spinBox = qobject_cast<QSpinBox*>(sender());
@ -347,7 +347,7 @@ void FlightMode::phaseREValue_editingFinished()
}
}
void FlightMode::phaseREUse_currentIndexChanged(int index)
void FlightModePanel::phaseREUse_currentIndexChanged(int index)
{
if (!lock) {
lock = true;
@ -365,7 +365,7 @@ void FlightMode::phaseREUse_currentIndexChanged(int index)
}
}
void FlightMode::phaseTrimUse_currentIndexChanged(int index)
void FlightModePanel::phaseTrimUse_currentIndexChanged(int index)
{
if (!lock) {
QComboBox *comboBox = qobject_cast<QComboBox*>(sender());
@ -387,7 +387,7 @@ void FlightMode::phaseTrimUse_currentIndexChanged(int index)
}
}
void FlightMode::phaseTrim_valueChanged()
void FlightModePanel::phaseTrim_valueChanged()
{
if (!lock) {
QSpinBox *spinBox = qobject_cast<QSpinBox*>(sender());
@ -402,7 +402,7 @@ void FlightMode::phaseTrim_valueChanged()
}
}
void FlightMode::phaseTrimSlider_valueChanged()
void FlightModePanel::phaseTrimSlider_valueChanged()
{
if (!lock) {
QSlider *slider = qobject_cast<QSlider*>(sender());
@ -419,14 +419,14 @@ void FlightMode::phaseTrimSlider_valueChanged()
/**********************************************************/
FlightModes::FlightModes(QWidget * parent, ModelData & model, GeneralSettings & generalSettings, FirmwareInterface * firmware):
FlightModesPanel::FlightModesPanel(QWidget * parent, ModelData & model, GeneralSettings & generalSettings, FirmwareInterface * firmware):
ModelPanel(parent, model, generalSettings, firmware),
modesCount(firmware->getCapability(FlightPhases))
modesCount(firmware->getCapability(FlightModes))
{
QGridLayout * gridLayout = new QGridLayout(this);
tabWidget = new QTabWidget(this);
for (int i=0; i<modesCount; i++) {
FlightMode *tab = new FlightMode(tabWidget, model, i, generalSettings, firmware);
FlightModePanel *tab = new FlightModePanel(tabWidget, model, i, generalSettings, firmware);
tab->setProperty("index", i);
panels << tab;
connect(tab, SIGNAL(modified()), this, SLOT(onPhaseModified()));
@ -437,16 +437,16 @@ FlightModes::FlightModes(QWidget * parent, ModelData & model, GeneralSettings &
connect(tabWidget, SIGNAL(currentChanged(int)), this, SLOT(on_tabWidget_currentChanged(int)));
}
FlightModes::~FlightModes()
FlightModesPanel::~FlightModesPanel()
{
}
void FlightModes::onPhaseModified()
void FlightModesPanel::onPhaseModified()
{
emit modified();
}
QString FlightModes::getTabName(int index)
QString FlightModesPanel::getTabName(int index)
{
QString result = tr("Flight Mode %1").arg(index);
const char *name = model.phaseData[index].name;
@ -460,18 +460,18 @@ QString FlightModes::getTabName(int index)
return result;
}
void FlightModes::onPhaseNameChanged()
void FlightModesPanel::onPhaseNameChanged()
{
int index = sender()->property("index").toInt();
tabWidget->setTabText(index, getTabName(index));
}
void FlightModes::update()
void FlightModesPanel::update()
{
on_tabWidget_currentChanged(tabWidget->currentIndex());
}
void FlightModes::on_tabWidget_currentChanged(int index)
void FlightModesPanel::on_tabWidget_currentChanged(int index)
{
panels[index]->update();
}

14
companion/src/modeledit/flightmodes.h
View file

@ -13,13 +13,13 @@ namespace Ui {
class FlightMode;
}
class FlightMode : public ModelPanel
class FlightModePanel : public ModelPanel
{
Q_OBJECT
public:
FlightMode(QWidget *parent, ModelData &model, int modeIdx, GeneralSettings & generalSettings, FirmwareInterface * firmware);
virtual ~FlightMode();
FlightModePanel(QWidget *parent, ModelData &model, int modeIdx, GeneralSettings & generalSettings, FirmwareInterface * firmware);
virtual ~FlightModePanel();
virtual void update();
@ -61,13 +61,13 @@ class FlightMode : public ModelPanel
};
class FlightModes : public ModelPanel
class FlightModesPanel : public ModelPanel
{
Q_OBJECT
public:
FlightModes(QWidget *parent, ModelData & model, GeneralSettings & generalSettings, FirmwareInterface * firmware);
virtual ~FlightModes();
FlightModesPanel(QWidget *parent, ModelData & model, GeneralSettings & generalSettings, FirmwareInterface * firmware);
virtual ~FlightModesPanel();
virtual void update();
@ -80,7 +80,7 @@ class FlightModes : public ModelPanel
int modesCount;
QTabWidget *tabWidget;
QString getTabName(int index);
QVector<FlightMode *> panels;
QVector<FlightModePanel *> panels;
};

4
companion/src/modeledit/mixerdialog.cpp
View file

@ -55,7 +55,7 @@ MixerDialog::MixerDialog(QWidget *parent, ModelData & model, MixData *mixdata, G
ui->mixerName->setValidator(new QRegExpValidator(rx, this));
ui->mixerName->setText(md->name);
if (!firmware->getCapability(FlightPhases)) {
if (!firmware->getCapability(FlightModes)) {
ui->label_phases->hide();
for (int i=0; i<9; i++) {
lb_fp[i]->hide();
@ -70,7 +70,7 @@ MixerDialog::MixerDialog(QWidget *parent, ModelData & model, MixData *mixdata, G
}
mask <<= 1;
}
for (int i=firmware->getCapability(FlightPhases); i<9;i++) {
for (int i=firmware->getCapability(FlightModes); i<9;i++) {
lb_fp[i]->hide();
cb_fp[i]->hide();
}

2
companion/src/modeledit/modeledit.cpp
View file

@ -29,7 +29,7 @@ ModelEdit::ModelEdit(QWidget * parent, RadioData & radioData, int modelId, Firmw
SetupPanel * setupPanel = new SetupPanel(this, model, generalSettings, firmware);
addTab(setupPanel, tr("Setup"));
addTab(new HeliPanel(this, model, generalSettings, firmware), tr("Heli"));
addTab(new FlightModes(this, model, generalSettings, firmware), tr("Flight Modes"));
addTab(new FlightModesPanel(this, model, generalSettings, firmware), tr("Flight Modes"));
addTab(new InputsPanel(this, model, generalSettings, firmware), tr("Inputs"));
addTab(new MixesPanel(this, model, generalSettings, firmware), tr("Mixes"));
Channels * chnPanel = new Channels(this, model, generalSettings, firmware);

31
companion/src/printdialog.cpp
View file

@ -45,7 +45,7 @@ PrintDialog::PrintDialog(QWidget *parent, FirmwareInterface * firmware, GeneralS
}
printSetup();
if (gvars) {
te->append(printPhases()+"<br>");
te->append(printFlightModes()+"<br>");
}
printInputs();
printMixes();
@ -112,7 +112,7 @@ QString PrintDialog::fv(const QString name, const QString value)
void PrintDialog::printSetup()
{
QString str = "<a name=1></a><table border=1 cellspacing=0 cellpadding=3 width=\"100%\">";
str.append(QString("<tr><td colspan=%1 ><table border=0 width=\"100%\"><tr><td><h1>").arg((firmware->getCapability(FlightPhases) && !gvars) ? 2 : 1));
str.append(QString("<tr><td colspan=%1 ><table border=0 width=\"100%\"><tr><td><h1>").arg((firmware->getCapability(FlightModes) && !gvars) ? 2 : 1));
str.append(g_model->name);
str.append("&nbsp;(");
str.append(firmware->getEepromInterface()->getName());
@ -133,18 +133,18 @@ void PrintDialog::printSetup()
str.append("</td></tr></table></td>");
if (!gvars) {
str.append("<td width=\"380\">");
str.append(printPhases());
str.append(printFlightModes());
str.append("</td>");
}
str.append("</tr></table><br>");
te->append(str);
}
QString PrintDialog::printPhases()
QString PrintDialog::printFlightModes()
{
QString str="";
str.append(QString("<table border=1 cellspacing=0 cellpadding=3 width=\"100%\"><tr><td colspan=%1><h2>").arg(!gvars ? 8+firmware->getCapability(RotaryEncoders) : 8+gvarnum+firmware->getCapability(RotaryEncoders)));
str.append(tr("Flight modes Settings"));
str.append(tr("Flight modes"));
str.append("</h2></td></tr><tr><td style=\"border-style:none;\">&nbsp;</td><td colspan=2 align=center><b>");
str.append(tr("Fades")+"</b></td>");
str.append("<td colspan=4 align=center><b>"+tr("Trims")+"</b></td>");
@ -170,8 +170,7 @@ QString PrintDialog::printPhases()
str.append(QString("<td align=\"center\"><b>RE%1</b></td>").arg((i==0 ? 'A': 'B')));
}
str.append("</tr>");
for (int i=0; i<firmware->getCapability(FlightPhases); i++) {
for (int i=0; i<firmware->getCapability(FlightModes); i++) {
PhaseData *pd=&g_model->phaseData[i];
str.append("<tr><td><b>"+tr("FM")+QString("%1</b> <font size=+1 face='Courier New' color=green>%2</font></td>").arg(i).arg(pd->name));
str.append(QString("<td align=\"right\"><font size=+1 face='Courier New' color=green>%1</font></td>").arg((qreal)pd->fadeIn/firmware->getCapability(SlowScale)));
@ -254,29 +253,29 @@ void PrintDialog::printInputs()
}
if (ed->curve.value) str += " " + Qt::escape(ed->curve.toString());
if (firmware->getCapability(FlightPhases)) {
if (firmware->getCapability(FlightModes)) {
if(ed->phases) {
if (ed->phases!=(unsigned int)(1<<firmware->getCapability(FlightPhases))-1) {
if (ed->phases!=(unsigned int)(1<<firmware->getCapability(FlightModes))-1) {
unsigned int mask=1;
bool first = true;
bool multiple = false;
QString strPhases;
for (int j=0; j<firmware->getCapability(FlightPhases);j++) {
QString strModes;
for (int j=0; j<firmware->getCapability(FlightModes);j++) {
if (!(ed->phases & mask)) {
//PhaseData *pd = &g_model->phaseData[j];
const char * pdName = g_model->phaseData[j].name;
if (first) {
strPhases += Qt::escape(QString("%1").arg(getPhaseName(j+1,pdName)));
strModes += Qt::escape(QString("%1").arg(getPhaseName(j+1,pdName)));
first = false;
} else {
strPhases += Qt::escape(QString(", %1").arg(getPhaseName(j+1, pdName)));
strModes += Qt::escape(QString(", %1").arg(getPhaseName(j+1, pdName)));
multiple = true;
}
}
mask <<= 1;
}
if (!strPhases.isEmpty()) {
str += " " + tr(multiple?"Flight modes":"Flight mode") + "(" + strPhases + ")";
if (!strModes.isEmpty()) {
str += " " + tr(multiple?"Flight modes":"Flight mode") + "(" + strModes + ")";
}
} else {
str += tr("DISABLED")+QString(" !!!");
@ -613,7 +612,7 @@ void PrintDialog::printSwitches()
void PrintDialog::printGvars()
{
if (!firmware->getCapability(GvarsFlightPhases) && (gvars && firmware->getCapability(Gvars))) {
if (!firmware->getCapability(GvarsFlightModes) && (gvars && firmware->getCapability(Gvars))) {
QString str = "<table border=1 cellspacing=0 cellpadding=3 width=\"100%\">";
str.append("<tr><td><h2>"+tr("Global Variables")+"</h2></td></tr>");
str.append("<tr><td><table border=1 cellspacing=0 cellpadding=3 width=100>");

2
companion/src/printdialog.h
View file

@ -32,7 +32,7 @@ private:
unsigned int gvarnum;
void printSetup();
QString printPhases();
QString printFlightModes();
void printInputs();
void printMixes();
void printLimits();

8
companion/src/simulation/simulatordialog.cpp
View file

@ -600,7 +600,7 @@ void SimulatorDialog9X::getValues()
void SimulatorDialog9X::saveSwitches(void)
{
qDebug() << "SimulatorDialog9X::saveSwitches()";
// qDebug() << "SimulatorDialog9X::saveSwitches()";
switchstatus=ui->switchTHR->isChecked();
switchstatus<<=1;
switchstatus+=(ui->switchRUD->isChecked()&0x1);
@ -620,7 +620,7 @@ void SimulatorDialog9X::saveSwitches(void)
void SimulatorDialog9X::restoreSwitches(void)
{
qDebug() << "SimulatorDialog9X::restoreSwitches()";
// qDebug() << "SimulatorDialog9X::restoreSwitches()";
ui->switchAIL->setChecked(switchstatus & 0x1);
switchstatus >>=1;
ui->switchELE->setChecked(switchstatus & 0x1);
@ -705,7 +705,7 @@ void SimulatorDialogTaranis::getValues()
void SimulatorDialogTaranis::saveSwitches(void)
{
qDebug() << "SimulatorDialogTaranis::saveSwitches()";
// qDebug() << "SimulatorDialogTaranis::saveSwitches()";
switchstatus=ui->switchA->value();
switchstatus<<=2;
switchstatus+=ui->switchB->value();
@ -725,7 +725,7 @@ void SimulatorDialogTaranis::saveSwitches(void)
void SimulatorDialogTaranis::restoreSwitches(void)
{
qDebug() << "SimulatorDialogTaranis::restoreSwitches()";
// qDebug() << "SimulatorDialogTaranis::restoreSwitches()";
ui->switchH->setValue(switchstatus & 0x3);
switchstatus>>=2;
ui->switchG->setValue(switchstatus & 0x3);

2
companion/src/xmlinterface.cpp
View file

@ -155,7 +155,7 @@ void saveModel(ModelData & m, model & xm)
phases xphases;
phases::phase_sequence & phases_sequence (xphases.phase());
for (int i=0; i<C9X_MAX_PHASES; i++) {
for (int i=0; i<C9X_MAX_FLIGHT_MODES; i++) {
PhaseData & p = m.phaseData[i];
if (i == 0 || p.swtch.type!=SWITCH_TYPE_NONE) {
TrimType xtrim[4];

4
radio/src/Makefile
View file

@ -1078,7 +1078,7 @@ MSG_CLEANING = Cleaning project:
# Combine all necessary flags and optional flags.
# Add target processor to flags.
ARMCPPFLAGS = -c -mcpu=$(MCU) -mthumb -fomit-frame-pointer -fverbose-asm -Wa,-ahlms=opentx.lst -DRUN_FROM_FLASH=1 -O$(OPT) $(CPPFLAGS) $(INCFLAGS) $(EXTRAINCFLAGS) $(GENDEPFLAGS)
ARMCPPFLAGS = -c -mcpu=$(MCU) -mthumb -fomit-frame-pointer -fverbose-asm -Wa,-ahlms=opentx.lst -DRUN_FROM_FLASH=1 -O$(OPT) $(CPPFLAGS) -fdata-sections -ffunction-sections $(INCFLAGS) $(EXTRAINCFLAGS) $(GENDEPFLAGS)
AVRCPPFLAGS = -mmcu=$(MCU) -I. -x c++ -O$(OPT) $(CPPFLAGS) $(INCFLAGS) $(EXTRAINCFLAGS) $(GENDEPFLAGS) -fwhole-program
ifeq ($(ARCH), AVR)
@ -1349,7 +1349,7 @@ OBJS = $(TMP:.s=.o)
@echo
@echo $(MSG_COMPILING) $@
$(CC) $(ARMCPPFLAGS) $< -o allsrc.o
$(CC) $(OBJS) allsrc.o -mcpu=cortex-m3 -mthumb -nostartfiles -lm -T$(LDSCRIPT) -Wl,-Map=$(TARGET).map,--cref,--no-warn-mismatch -o $@
$(CC) $(OBJS) allsrc.o -mcpu=cortex-m3 -mthumb -nostartfiles -lm -T$(LDSCRIPT) -Wl,-Map=$(TARGET).map,--cref,--no-warn-mismatch,--gc-sections -o $@
endif
# Target: clean project.

4
radio/src/audio_arm.cpp
View file

@ -333,7 +333,7 @@ void getLogicalSwitchAudioFile(char * filename, int index, unsigned int event)
{
char * str = getModelPath(filename);
int len = STR_VSWITCHES[0];
strncpy(str, &STR_VSWITCHES[1+len*(index+SWSRC_FIRST_CSW-1)], len);
strncpy(str, &STR_VSWITCHES[1+len*(index+SWSRC_FIRST_LOGICAL_SWITCH-1)], len);
str += len;
strcpy(str, suffixes[event]);
strcat(str, SOUNDS_EXT);
@ -369,7 +369,7 @@ void referenceModelAudioFiles()
if (len < 5 || strcasecmp(fn+len-4, SOUNDS_EXT) || (fno.fattrib & AM_DIR)) continue;
// Phases Audio Files <phasename>-[on|off].wav
for (int i=0; i<MAX_PHASES && !found; i++) {
for (int i=0; i<MAX_FLIGHT_MODES && !found; i++) {
for (int event=0; event<2; event++) {
getPhaseAudioFile(path, i, event);
if (!strcasecmp(filename, fn)) {

2
radio/src/eeprom_conversions.cpp
View file

@ -225,7 +225,7 @@ PACK(typedef struct {
LogicalSwitchData_v215 customSw[NUM_LOGICAL_SWITCH];
CustomFnData_v215 funcSw[32];
SwashRingData swashR;
PhaseData_v215 phaseData[MAX_PHASES];
PhaseData_v215 phaseData[MAX_FLIGHT_MODES];
int8_t ppmFrameLength; // 0=22.5ms (10ms-30ms) 0.5ms increments
uint8_t thrTraceSrc;

8
radio/src/gtests.cpp
View file

@ -629,13 +629,13 @@ TEST(Mixer, SlowOnPhase)
g_model.mixData[0].speedDown = SLOW_STEP*5;
s_mixer_first_run_done = true;
s_perout_flight_phase = 0;
s_perout_flight_mode = 0;
perOut(e_perout_mode_normal, 0);
EXPECT_EQ(chans[0], 0);
CHECK_SLOW_MOVEMENT(0, +1, 250);
s_perout_flight_phase = 1;
s_perout_flight_mode = 1;
CHECK_SLOW_MOVEMENT(0, -1, 250);
}
@ -663,11 +663,11 @@ TEST(Mixer, SlowOnSwitchAndPhase)
EXPECT_EQ(chans[0], 0);
simuSetSwitch(0, 1);
s_perout_flight_phase = 0;
s_perout_flight_mode = 0;
CHECK_SLOW_MOVEMENT(0, +1, 250);
simuSetSwitch(0, -1);
s_perout_flight_phase = 1;
s_perout_flight_mode = 1;
CHECK_SLOW_MOVEMENT(0, -1, 250);
}
#endif

77
radio/src/gui/menu_model.cpp
View file

@ -1067,7 +1067,7 @@ void menuModelSetup(uint8_t event)
div_t qr = div(timer->start, 60);
switch (m_posHorz) {
case 0:
CHECK_INCDEC_MODELVAR(event, timer->mode, SWSRC_FIRST, TMR_VAROFS+SWSRC_LAST-1/*--- which is OFF*/);
CHECK_INCDEC_MODELVAR(event, timer->mode, SWSRC_FIRST, TMR_VAROFS+SWSRC_LAST-1);
break;
case 1:
CHECK_INCDEC_MODELVAR_ZERO(event, qr.quot, 59);
@ -1108,7 +1108,7 @@ void menuModelSetup(uint8_t event)
s_editMode = 0;
if (event==EVT_KEY_LONG(KEY_ENTER)) {
s_noHi = NO_HI_LEN;
for (uint8_t i=0; i<MAX_PHASES; i++) {
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
memclear(&g_model.phaseData[i], TRIMS_ARRAY_SIZE);
}
eeDirty(EE_MODEL);
@ -1757,7 +1757,7 @@ uint8_t editDelay(const uint8_t y, const uint8_t event, const uint8_t attr, cons
void displayFlightModes(uint8_t x, uint8_t y, FlightModesType value)
{
uint8_t p = MAX_PHASES;
uint8_t p = MAX_FLIGHT_MODES;
do {
--p;
if (!(value & (1<<p)))
@ -1781,7 +1781,7 @@ FlightModesType editFlightModes(uint8_t x, uint8_t y, uint8_t event, FlightModes
bool expoMenu = (x==EXPO_ONE_2ND_COLUMN-5*FW);
#endif
for (uint8_t p=0; p<MAX_PHASES; p++) {
for (uint8_t p=0; p<MAX_FLIGHT_MODES; p++) {
#if defined(CPUARM) && LCD_W < 212
if (expoMenu && ((attr && p < posHorz-4) || (x > EXPO_ONE_2ND_COLUMN-FW)))
continue;
@ -1835,14 +1835,14 @@ bool isTrimModeAvailable(int mode)
void menuModelFlightModesAll(uint8_t event)
{
MENU(STR_MENUFLIGHTPHASES, menuTabModel, e_FlightModesAll, 1+MAX_PHASES+1, {0, NAVIGATION_LINE_BY_LINE|(ITEM_PHASES_LAST-5), NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, 0});
MENU(STR_MENUFLIGHTPHASES, menuTabModel, e_FlightModesAll, 1+MAX_FLIGHT_MODES+1, {0, NAVIGATION_LINE_BY_LINE|(ITEM_PHASES_LAST-5), NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, NAVIGATION_LINE_BY_LINE|ITEM_PHASES_LAST, 0});
int8_t sub = m_posVert - 1;
horzpos_t posHorz = m_posHorz;
if (sub==0 && posHorz > 0) { posHorz += 5; }
if (sub<MAX_PHASES && posHorz>=0) {
if (sub<MAX_FLIGHT_MODES && posHorz>=0) {
displayColumnHeader(STR_PHASES_HEADERS, posHorz);
}
@ -1850,11 +1850,11 @@ void menuModelFlightModesAll(uint8_t event)
uint8_t y = 1 + (i+1)*FH;
uint8_t k = i+s_pgOfs;
if (k==MAX_PHASES) {
if (k==MAX_FLIGHT_MODES) {
// last line available - add the "check trims" line
lcd_putsLeft((LCD_LINES-1)*FH+1, STR_CHECKTRIMS);
putsFlightPhase(OFS_CHECKTRIMS, (LCD_LINES-1)*FH+1, s_perout_flight_phase+1);
if (sub==MAX_PHASES && !trimsCheckTimer) {
putsFlightMode(OFS_CHECKTRIMS, (LCD_LINES-1)*FH+1, s_perout_flight_mode+1);
if (sub==MAX_FLIGHT_MODES && !trimsCheckTimer) {
lcd_status_line();
}
return;
@ -1862,7 +1862,7 @@ void menuModelFlightModesAll(uint8_t event)
PhaseData *p = phaseAddress(k);
putsFlightPhase(0, y, k+1, (getFlightPhase()==k ? BOLD : 0) | ((sub==k && m_posHorz<0) ? INVERS : 0));
putsFlightMode(0, y, k+1, (getFlightPhase()==k ? BOLD : 0) | ((sub==k && m_posHorz<0) ? INVERS : 0));
for (uint8_t j=0; j<ITEM_PHASES_COUNT; j++) {
uint8_t attr = ((sub==k && posHorz==j) ? ((s_editMode>0) ? BLINK|INVERS : INVERS) : 0);
@ -1878,7 +1878,7 @@ void menuModelFlightModesAll(uint8_t event)
}
else {
putsSwitches((5+LEN_FP_NAME)*FW+FW/2, y, p->swtch, attr);
if (active) CHECK_INCDEC_MODELSWITCH(event, p->swtch, SWSRC_FIRST, SWSRC_LAST);
if (active) CHECK_INCDEC_MODELSWITCH(event, p->swtch, SWSRC_FIRST_SHORT_LIST, SWSRC_LAST_SHORT_LIST);
}
break;
@ -1891,7 +1891,7 @@ void menuModelFlightModesAll(uint8_t event)
putsTrimMode((4+LEN_FP_NAME)*FW+j*(5*FW/2), y, k, t, attr);
if (active) {
trim_t & v = p->trim[t];
v.mode = checkIncDec(event, v.mode==TRIM_MODE_NONE ? -1 : v.mode, -1, 2*MAX_PHASES-1, EE_MODEL, isTrimModeAvailable);
v.mode = checkIncDec(event, v.mode==TRIM_MODE_NONE ? -1 : v.mode, -1, 2*MAX_FLIGHT_MODES-1, EE_MODEL, isTrimModeAvailable);
}
}
break;
@ -1933,7 +1933,7 @@ enum menuModelPhaseItems {
void menuModelPhaseOne(uint8_t event)
{
PhaseData *phase = phaseAddress(s_currIdx);
putsFlightPhase(13*FW, 0, s_currIdx+1, (getFlightPhase()==s_currIdx ? BOLD : 0));
putsFlightMode(13*FW, 0, s_currIdx+1, (getFlightPhase()==s_currIdx ? BOLD : 0));
#if defined(GVARS) && !defined(PCBSTD)
static const pm_uint8_t mstate_tab_phase1[] PROGMEM = {0, 0, 0, (uint8_t)-1, 1, 1, 1, 1, 1};
@ -1979,7 +1979,7 @@ void menuModelPhaseOne(uint8_t event)
if (attr && m_posHorz==t && ((editMode>0) || p1valdiff)) {
int16_t v = getRawTrimValue(s_currIdx, t);
if (v < TRIM_EXTENDED_MAX) v = TRIM_EXTENDED_MAX;
v = checkIncDec(event, v, TRIM_EXTENDED_MAX, TRIM_EXTENDED_MAX+MAX_PHASES-1, EE_MODEL);
v = checkIncDec(event, v, TRIM_EXTENDED_MAX, TRIM_EXTENDED_MAX+MAX_FLIGHT_MODES-1, EE_MODEL);
if (checkIncDec_Ret) {
if (v == TRIM_EXTENDED_MAX) v = 0;
setTrimValue(s_currIdx, t, v);
@ -2004,7 +2004,7 @@ void menuModelPhaseOne(uint8_t event)
int16_t v = phaseAddress(s_currIdx)->rotaryEncoders[t];
#endif
if (v < ROTARY_ENCODER_MAX) v = ROTARY_ENCODER_MAX;
v = checkIncDec(event, v, ROTARY_ENCODER_MAX, ROTARY_ENCODER_MAX+MAX_PHASES-1, EE_MODEL);
v = checkIncDec(event, v, ROTARY_ENCODER_MAX, ROTARY_ENCODER_MAX+MAX_FLIGHT_MODES-1, EE_MODEL);
if (checkIncDec_Ret) {
if (v == ROTARY_ENCODER_MAX) v = 0;
#if ROTARY_ENCODERS > 2
@ -2048,14 +2048,14 @@ void menuModelPhaseOne(uint8_t event)
if (v > GVAR_MAX) {
uint8_t p = v - GVAR_MAX - 1;
if (p >= s_currIdx) p++;
putsFlightPhase(11*FW, y, p+1, posHorz==1 ? attr : 0);
putsFlightMode(11*FW, y, p+1, posHorz==1 ? attr : 0);
}
else {
lcd_putsAtt(11*FW, y, STR_OWN, posHorz==1 ? attr : 0);
}
if (attr && s_currIdx>0 && posHorz==1 && (editMode>0 || p1valdiff)) {
if (v < GVAR_MAX) v = GVAR_MAX;
v = checkIncDec(event, v, GVAR_MAX, GVAR_MAX+MAX_PHASES-1, EE_MODEL);
v = checkIncDec(event, v, GVAR_MAX, GVAR_MAX+MAX_FLIGHT_MODES-1, EE_MODEL);
if (checkIncDec_Ret) {
if (v == GVAR_MAX) v = 0;
phase->gvars[idx] = v;
@ -2095,20 +2095,20 @@ void menuModelPhaseOne(uint8_t event)
void menuModelFlightModesAll(uint8_t event)
{
SIMPLE_MENU(STR_MENUFLIGHTPHASES, menuTabModel, e_FlightModesAll, 1+MAX_PHASES+1);
SIMPLE_MENU(STR_MENUFLIGHTPHASES, menuTabModel, e_FlightModesAll, 1+MAX_FLIGHT_MODES+1);
int8_t sub = m_posVert - 1;
switch (event) {
CASE_EVT_ROTARY_BREAK
case EVT_KEY_FIRST(KEY_ENTER):
if (sub == MAX_PHASES) {
if (sub == MAX_FLIGHT_MODES) {
s_editMode = 0;
trimsCheckTimer = 200; // 2 seconds
}
// no break
case EVT_KEY_FIRST(KEY_RIGHT):
if (sub >= 0 && sub < MAX_PHASES) {
if (sub >= 0 && sub < MAX_FLIGHT_MODES) {
s_currIdx = sub;
pushMenu(menuModelPhaseOne);
}
@ -2116,7 +2116,7 @@ void menuModelFlightModesAll(uint8_t event)
}
uint8_t att;
for (uint8_t i=0; i<MAX_PHASES; i++) {
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
#if defined(CPUARM)
int8_t y = 1 + (1+i-s_pgOfs)*FH;
if (y<1*FH+1 || y>(LCD_LINES-1)*FH+1) continue;
@ -2126,9 +2126,9 @@ void menuModelFlightModesAll(uint8_t event)
att = (i==sub ? INVERS : 0);
PhaseData *p = phaseAddress(i);
#if ROTARY_ENCODERS > 2
putsFlightPhase(0, y, i+1, att|CONDENSED|(getFlightPhase()==i ? BOLD : 0));
putsFlightMode(0, y, i+1, att|CONDENSED|(getFlightPhase()==i ? BOLD : 0));
#else
putsFlightPhase(0, y, i+1, att|(getFlightPhase()==i ? BOLD : 0));
putsFlightMode(0, y, i+1, att|(getFlightPhase()==i ? BOLD : 0));
#endif
lcd_putsnAtt(4*FW+NAME_OFS, y, p->name, sizeof(p->name), ZCHAR);
@ -2153,12 +2153,12 @@ void menuModelFlightModesAll(uint8_t event)
}
#if defined(CPUARM)
if (s_pgOfs != MAX_PHASES-(LCD_LINES-2)) return;
if (s_pgOfs != MAX_FLIGHT_MODES-(LCD_LINES-2)) return;
#endif
lcd_putsLeft((LCD_LINES-1)*FH+1, STR_CHECKTRIMS);
putsFlightPhase(OFS_CHECKTRIMS, (LCD_LINES-1)*FH+1, s_perout_flight_phase+1);
if (sub==MAX_PHASES && !trimsCheckTimer) {
putsFlightMode(OFS_CHECKTRIMS, (LCD_LINES-1)*FH+1, s_perout_flight_mode+1);
if (sub==MAX_FLIGHT_MODES && !trimsCheckTimer) {
lcd_status_line();
}
}
@ -2910,7 +2910,7 @@ void menuModelExpoOne(uint8_t event)
putsMixerSource(7*FW+FW/2, 0, MIXSRC_Rud+ed->chn, 0);
#endif
SUBMENU(STR_MENUINPUTS, EXPO_FIELD_MAX, {CASE_PCBTARANIS(0) IF_CPUARM(0) CASE_PCBTARANIS(0) CASE_PCBTARANIS((ed->srcRaw >= MIXSRC_FIRST_TELEM ? (uint8_t)0 : (uint8_t)HIDDEN_ROW)) 0, CASE_PCBTARANIS(0) CASE_9X(0) IF_CURVES(CURVE_ROWS) IF_FLIGHT_MODES((MAX_PHASES-1) | NAVIGATION_LINE_BY_LINE) 0 /*, ...*/});
SUBMENU(STR_MENUINPUTS, EXPO_FIELD_MAX, {CASE_PCBTARANIS(0) IF_CPUARM(0) CASE_PCBTARANIS(0) CASE_PCBTARANIS((ed->srcRaw >= MIXSRC_FIRST_TELEM ? (uint8_t)0 : (uint8_t)HIDDEN_ROW)) 0, CASE_PCBTARANIS(0) CASE_9X(0) IF_CURVES(CURVE_ROWS) IF_FLIGHT_MODES((MAX_FLIGHT_MODES-1) | NAVIGATION_LINE_BY_LINE) 0 /*, ...*/});
SET_SCROLLBAR_X(EXPO_ONE_2ND_COLUMN+10*FW);
@ -3111,11 +3111,11 @@ void menuModelMixOne(uint8_t event)
#else
if (m_posVert == MIX_FIELD_TRIM && md2->srcRaw > NUM_STICKS)
#endif
SUBMENU_NOTITLE(MIX_FIELD_COUNT, {IF_CPUARM(0) 0, 0, 0, CASE_9X(0) IF_CURVES(0) IF_FLIGHT_MODES((MAX_PHASES-1) | NAVIGATION_LINE_BY_LINE) 0, 0 /*, ...*/})
SUBMENU_NOTITLE(MIX_FIELD_COUNT, {IF_CPUARM(0) 0, 0, 0, CASE_9X(0) IF_CURVES(0) IF_FLIGHT_MODES((MAX_FLIGHT_MODES-1) | NAVIGATION_LINE_BY_LINE) 0, 0 /*, ...*/})
else
SUBMENU_NOTITLE(MIX_FIELD_COUNT, {IF_CPUARM(0) 0, 0, 0, CASE_9X(1) IF_CURVES(1) IF_FLIGHT_MODES((MAX_PHASES-1) | NAVIGATION_LINE_BY_LINE) 0, 0 /*, ...*/});
SUBMENU_NOTITLE(MIX_FIELD_COUNT, {IF_CPUARM(0) 0, 0, 0, CASE_9X(1) IF_CURVES(1) IF_FLIGHT_MODES((MAX_FLIGHT_MODES-1) | NAVIGATION_LINE_BY_LINE) 0, 0 /*, ...*/});
#else
SUBMENU_NOTITLE(MIX_FIELD_COUNT, {IF_CPUARM(0) 0, 0, 0, CASE_9X(1) CASE_PCBTARANIS(0) IF_CURVES(1) IF_FLIGHT_MODES((MAX_PHASES-1) | NAVIGATION_LINE_BY_LINE) 0, 0 /*, ...*/});
SUBMENU_NOTITLE(MIX_FIELD_COUNT, {IF_CPUARM(0) 0, 0, 0, CASE_9X(1) CASE_PCBTARANIS(0) IF_CURVES(1) IF_FLIGHT_MODES((MAX_FLIGHT_MODES-1) | NAVIGATION_LINE_BY_LINE) 0, 0 /*, ...*/});
#endif
#if MENU_COLUMNS > 1
@ -3314,7 +3314,7 @@ static uint8_t s_copySrcCh;
#define EXPO_LINE_WEIGHT_POS 7*FW+1
#define EXPO_LINE_EXPO_POS 11*FW
#define EXPO_LINE_SWITCH_POS 11*FW+4
#if MAX_PHASES == 6
#if MAX_FLIGHT_MODES == 6
#define EXPO_LINE_SIDE_POS 15*FW
#else
#define EXPO_LINE_SIDE_POS 15*FW+2
@ -4102,7 +4102,7 @@ void onGVARSMenu(const char *result)
eeDirty(EE_MODEL);
}
else if (result == STR_CLEAR) {
for (int i=0; i<MAX_PHASES; i++) {
for (int i=0; i<MAX_FLIGHT_MODES; i++) {
g_model.phaseData[i].gvars[sub] = 0;
}
eeDirty(EE_MODEL);
@ -4127,7 +4127,7 @@ void menuModelGVars(uint8_t event)
menuTitle = STR_MENUGLOBALVARS;
}
MENU_FLAGS(menuTitle, menuTabModel, e_GVars, first2seconds ? CHECK_FLAG_NO_SCREEN_INDEX : 0, 1+MAX_GVARS, {0, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES, NAVIGATION_LINE_BY_LINE|MAX_PHASES});
MENU_FLAGS(menuTitle, menuTabModel, e_GVars, first2seconds ? CHECK_FLAG_NO_SCREEN_INDEX : 0, 1+MAX_GVARS, {0, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES, NAVIGATION_LINE_BY_LINE|MAX_FLIGHT_MODES});
uint8_t sub = m_posVert - 1;
@ -4146,7 +4146,7 @@ void menuModelGVars(uint8_t event)
if (g_model.gvars[i].popup) lcd_putc(3*FW, y, '!');
putsStrIdx(0, y, STR_GV, i+1, (sub==i && m_posHorz<0) ? INVERS : 0);
for (uint8_t j=0; j<1+MAX_PHASES; j++) {
for (uint8_t j=0; j<1+MAX_FLIGHT_MODES; j++) {
LcdFlags attr = ((sub==i && m_posHorz==j) ? ((s_editMode>0) ? BLINK|INVERS : INVERS) : 0);
xcoord_t x = GVARS_FM_COLUMN(j-1);
@ -4170,8 +4170,8 @@ void menuModelGVars(uint8_t event)
if (v > GVAR_MAX) {
uint8_t p = v - GVAR_MAX - 1;
if (p >= j-1) p++;
putsFlightPhase(x-15, y, p+1, attr|SMLSIZE);
vmin = GVAR_MAX+1; vmax = GVAR_MAX+MAX_PHASES-1;
putsFlightMode(x-15, y, p+1, attr|SMLSIZE);
vmin = GVAR_MAX+1; vmax = GVAR_MAX+MAX_FLIGHT_MODES-1;
}
else {
if (abs(v) >= 100)
@ -4967,10 +4967,11 @@ void menuModelCustomFunctions(uint8_t event)
{
INCDEC_DECLARE_VARS();
int16_t val_displayed = CFN_PARAM(sd);
int8_t val_min = 0;
#if defined(CPUARM)
int16_t val_min = 0;
int16_t val_max = 255;
#else
int8_t val_min = 0;
uint8_t val_max = 255;
#endif
if (func == FUNC_SAFETY_CHANNEL) {
@ -5084,7 +5085,7 @@ void menuModelCustomFunctions(uint8_t event)
switch (CFN_GVAR_MODE(sd)) {
case FUNC_ADJUST_GVAR_CONSTANT:
val_displayed = (int8_t)CFN_PARAM(sd);
val_min = -125; val_max = 125;
val_min = -CFN_GVAR_CST_MAX; val_max = +CFN_GVAR_CST_MAX;
lcd_outdezAtt(MODEL_CUSTOM_FUNC_3RD_COLUMN, y, val_displayed, attr|LEFT);
break;
case FUNC_ADJUST_GVAR_SOURCE:

12
radio/src/gui/menus.cpp
View file

@ -1132,7 +1132,7 @@ int8_t switchMenuItem(uint8_t x, uint8_t y, int8_t value, LcdFlags attr, uint8_t
{
lcd_putsColumnLeft(x, y, STR_SWITCH);
putsSwitches(x, y, value, attr);
if (attr) CHECK_INCDEC_MODELSWITCH(event, value, SWSRC_FIRST, SWSRC_LAST);
if (attr) CHECK_INCDEC_MODELSWITCH(event, value, SWSRC_FIRST_SHORT_LIST, SWSRC_LAST_SHORT_LIST);
return value;
}
@ -1152,11 +1152,11 @@ int16_t gvarMenuItem(uint8_t x, uint8_t y, int16_t value, int16_t min, int16_t m
s_editMode = !s_editMode;
#if defined(CPUARM)
if (attr & PREC1)
value = (GV_IS_GV_VALUE(value, min, max) ? GET_GVAR(value, min, max, s_perout_flight_phase)*10 : delta);
value = (GV_IS_GV_VALUE(value, min, max) ? GET_GVAR(value, min, max, s_perout_flight_mode)*10 : delta);
else
value = (GV_IS_GV_VALUE(value, min, max) ? GET_GVAR(value, min, max, s_perout_flight_phase) : delta);
value = (GV_IS_GV_VALUE(value, min, max) ? GET_GVAR(value, min, max, s_perout_flight_mode) : delta);
#else
value = (GV_IS_GV_VALUE(value, min, max) ? GET_GVAR(value, min, max, s_perout_flight_phase) : delta);
value = (GV_IS_GV_VALUE(value, min, max) ? GET_GVAR(value, min, max, s_perout_flight_mode) : delta);
#endif
eeDirty(EE_MODEL);
}
@ -1500,8 +1500,8 @@ bool isSwitchAvailable(int swtch)
swtch = -swtch;
}
if (swtch >= SWSRC_FIRST_CSW && swtch <= SWSRC_LAST_CSW) {
LogicalSwitchData * cs = cswAddress(swtch-SWSRC_FIRST_CSW);
if (swtch >= SWSRC_FIRST_LOGICAL_SWITCH && swtch <= SWSRC_LAST_LOGICAL_SWITCH) {
LogicalSwitchData * cs = cswAddress(swtch-SWSRC_FIRST_LOGICAL_SWITCH);
return (cs->func != LS_FUNC_NONE);
}

6
radio/src/gui/view_main.cpp
View file

@ -650,7 +650,7 @@ void menuMainView(uint8_t event)
{
// Flight Phase Name
uint8_t phase = s_perout_flight_phase;
uint8_t phase = s_perout_flight_mode;
lcd_putsnAtt(PHASE_X, PHASE_Y, g_model.phaseData[phase].name, sizeof(g_model.phaseData[phase].name), ZCHAR|PHASE_FLAGS);
// Model Name
@ -862,13 +862,13 @@ void menuMainView(uint8_t event)
putsStrIdx(BITMAP_X+FW, BITMAP_Y+FH-1, STR_GV, s_gvar_last+1);
lcd_putsnAtt(BITMAP_X+4*FW+FW/2, BITMAP_Y+FH-1, g_model.gvars[s_gvar_last].name, LEN_GVAR_NAME, ZCHAR);
lcd_putsAtt(BITMAP_X+FW, BITMAP_Y+2*FH+3, PSTR("[\010]"), BOLD);
lcd_outdezAtt(BITMAP_X+5*FW+FW/2, BITMAP_Y+2*FH+3, GVAR_VALUE(s_gvar_last, s_perout_flight_phase), BOLD);
lcd_outdezAtt(BITMAP_X+5*FW+FW/2, BITMAP_Y+2*FH+3, GVAR_VALUE(s_gvar_last, s_perout_flight_mode), BOLD);
#else
s_warning = STR_GLOBAL_VAR;
displayBox();
lcd_putsnAtt(16, 5*FH, g_model.gvars[s_gvar_last].name, LEN_GVAR_NAME, ZCHAR);
lcd_putsAtt(16+7*FW, 5*FH, PSTR("[\010]"), BOLD);
lcd_outdezAtt(16+7*FW+4*FW+FW/2, 5*FH, GVAR_VALUE(s_gvar_last, s_perout_flight_phase), BOLD);
lcd_outdezAtt(16+7*FW+4*FW+FW/2, 5*FH, GVAR_VALUE(s_gvar_last, s_perout_flight_mode), BOLD);
s_warning = NULL;
#endif
}

7
radio/src/lcd.cpp
View file

@ -1020,11 +1020,16 @@ void putsSwitches(xcoord_t x, uint8_t y, int8_t idx, LcdFlags att)
lcd_putcAtt(x-2, y, '!', att);
idx = -idx;
}
#if defined(CPUARM) && defined(FLIGHT_MODES)
if (idx >= SWSRC_FIRST_FLIGHT_MODE)
putsStrIdx(x, y, STR_FP, idx-SWSRC_FIRST_FLIGHT_MODE, att);
else
#endif
lcd_putsiAtt(x, y, STR_VSWITCHES, idx-1, att);
}
#if defined(FLIGHT_MODES)
void putsFlightPhase(xcoord_t x, uint8_t y, int8_t idx, LcdFlags att)
void putsFlightMode(xcoord_t x, uint8_t y, int8_t idx, LcdFlags att)
{
if (idx==0) { lcd_putsiAtt(x, y, STR_MMMINV, 0, att); return; }
if (idx < 0) { lcd_putcAtt(x-2, y, '!', att); idx = -idx; }

2
radio/src/lcd.h
View file

@ -178,7 +178,7 @@ void putsStrIdx(xcoord_t x, uint8_t y, const pm_char *str, uint8_t idx, LcdFlags
void putsModelName(xcoord_t x, uint8_t y, char *name, uint8_t id, LcdFlags att);
void putsSwitches(xcoord_t x, uint8_t y, int8_t swtch, LcdFlags att=0);
void putsMixerSource(xcoord_t x, uint8_t y, uint8_t idx, LcdFlags att=0);
void putsFlightPhase(xcoord_t x, uint8_t y, int8_t idx, LcdFlags att=0);
void putsFlightMode(xcoord_t x, uint8_t y, int8_t idx, LcdFlags att=0);
#if defined(PCBTARANIS) && !defined(BOOT)
void putsCurveRef(xcoord_t x, uint8_t y, CurveRef &curve, LcdFlags att);
#endif

27
radio/src/lua.cpp
View file

@ -741,6 +741,29 @@ static int luaModelSetOutput(lua_State *L)
return 0;
}
static int luaModelGetGlobalVariable(lua_State *L)
{
int idx = luaL_checkunsigned(L, 1);
int phase = luaL_checkunsigned(L, 2);
if (phase < MAX_FLIGHT_MODES && idx < MAX_GVARS)
lua_pushinteger(L, g_model.phaseData[phase].gvars[idx]);
else
lua_pushnil(L);
return 1;
}
static int luaModelSetGlobalVariable(lua_State *L)
{
int idx = luaL_checkunsigned(L, 1);
int phase = luaL_checkunsigned(L, 2);
int value = luaL_checkinteger(L, 3);
if (phase < MAX_FLIGHT_MODES && idx < MAX_GVARS && value >= -GVAR_LIMIT && value <= GVAR_LIMIT) {
g_model.phaseData[phase].gvars[idx] = value;
}
return 0;
}
static int luaPopupInput(lua_State *L)
{
uint8_t event = luaL_checkinteger(L, 2);
@ -849,6 +872,8 @@ static const luaL_Reg modelLib[] = {
{ "setCustomFunction", luaModelSetCustomFunction },
{ "getOutput", luaModelGetOutput },
{ "setOutput", luaModelSetOutput },
{ "getGlobalVariable", luaModelGetGlobalVariable },
{ "setGlobalVariable", luaModelSetGlobalVariable },
{ NULL, NULL } /* sentinel */
};
@ -901,7 +926,7 @@ void luaInit()
lua_registerint(L, "STICK_ELEVATOR", MIXSRC_Ele);
lua_registerint(L, "STICK_THROTTLE", MIXSRC_Thr);
lua_registerint(L, "STICK_AILERON", MIXSRC_Ail);
lua_registerint(L, "SWITCH_LAST", SWSRC_LAST_CSW);
lua_registerint(L, "SWITCH_LAST", SWSRC_LAST_LOGICAL_SWITCH);
lua_registerint(L, "EVT_MENU_BREAK", EVT_KEY_BREAK(KEY_MENU));
lua_registerint(L, "EVT_PAGE_BREAK", EVT_KEY_BREAK(KEY_PAGE));
lua_registerint(L, "EVT_ENTER_BREAK", EVT_KEY_BREAK(KEY_ENTER));

43
radio/src/myeeprom.h
View file

@ -73,7 +73,7 @@
#if defined(PCBTARANIS)
#define MAX_MODELS 60
#define NUM_CHNOUT 32 // number of real output channels CH1-CH32
#define MAX_PHASES 9
#define MAX_FLIGHT_MODES 9
#define MAX_MIXERS 64
#define MAX_EXPOS 64
#define NUM_LOGICAL_SWITCH 32 // number of custom switches
@ -86,7 +86,7 @@
#elif defined(CPUARM)
#define MAX_MODELS 60
#define NUM_CHNOUT 32 // number of real output channels CH1-CH32
#define MAX_PHASES 9
#define MAX_FLIGHT_MODES 9
#define MAX_MIXERS 64
#define MAX_EXPOS 32
#define NUM_LOGICAL_SWITCH 32 // number of custom switches
@ -97,7 +97,7 @@
#elif defined(CPUM2560) || defined(CPUM2561)
#define MAX_MODELS 30
#define NUM_CHNOUT 16 // number of real output channels CH1-CH16
#define MAX_PHASES 6
#define MAX_FLIGHT_MODES 6
#define MAX_MIXERS 32
#define MAX_EXPOS 16
#define NUM_LOGICAL_SWITCH 15 // number of custom switches
@ -108,7 +108,7 @@
#elif defined(CPUM128)
#define MAX_MODELS 30
#define NUM_CHNOUT 16 // number of real output channels CH1-CH16
#define MAX_PHASES 5
#define MAX_FLIGHT_MODES 5
#define MAX_MIXERS 32
#define MAX_EXPOS 14
#define NUM_LOGICAL_SWITCH 15 // number of custom switches
@ -119,7 +119,7 @@
#else
#define MAX_MODELS 16
#define NUM_CHNOUT 16 // number of real output channels CH1-CH16
#define MAX_PHASES 5
#define MAX_FLIGHT_MODES 5
#define MAX_MIXERS 32
#define MAX_EXPOS 14
#define NUM_LOGICAL_SWITCH 12 // number of custom switches
@ -522,9 +522,9 @@ PACK(typedef struct t_ExpoData {
#define limit_min_max_t int16_t
#define LIMIT_EXT_PERCENT 150
#define LIMIT_EXT_MAX (LIMIT_EXT_PERCENT*10)
#define LIMIT_MAX(lim) (GV_IS_GV_VALUE(lim->max, -LIMIT_EXT_MAX, LIMIT_EXT_MAX) ? GET_GVAR(lim->max, -LIMIT_EXT_MAX, LIMIT_EXT_MAX, s_perout_flight_phase)*10 : lim->max+1000)
#define LIMIT_MIN(lim) (GV_IS_GV_VALUE(lim->min, -LIMIT_EXT_MAX, LIMIT_EXT_MAX) ? GET_GVAR(lim->min, -LIMIT_EXT_MAX, LIMIT_EXT_MAX, s_perout_flight_phase)*10 : lim->min-1000)
#define LIMIT_OFS(lim) (GV_IS_GV_VALUE(lim->offset, -1000, 1000) ? GET_GVAR(lim->offset, -1000, 1000, s_perout_flight_phase)*10 : lim->offset)
#define LIMIT_MAX(lim) (GV_IS_GV_VALUE(lim->max, -LIMIT_EXT_MAX, LIMIT_EXT_MAX) ? GET_GVAR(lim->max, -LIMIT_EXT_MAX, LIMIT_EXT_MAX, s_perout_flight_mode)*10 : lim->max+1000)
#define LIMIT_MIN(lim) (GV_IS_GV_VALUE(lim->min, -LIMIT_EXT_MAX, LIMIT_EXT_MAX) ? GET_GVAR(lim->min, -LIMIT_EXT_MAX, LIMIT_EXT_MAX, s_perout_flight_mode)*10 : lim->min-1000)
#define LIMIT_OFS(lim) (GV_IS_GV_VALUE(lim->offset, -1000, 1000) ? GET_GVAR(lim->offset, -1000, 1000, s_perout_flight_mode)*10 : lim->offset)
#define LIMIT_MAX_RESX(lim) calc1000toRESX(LIMIT_MAX(lim))
#define LIMIT_MIN_RESX(lim) calc1000toRESX(LIMIT_MIN(lim))
#define LIMIT_OFS_RESX(lim) calc1000toRESX(LIMIT_OFS(lim))
@ -916,6 +916,7 @@ PACK(typedef struct t_CustomFnData { // Function Switches data
#define CFN_GVAR_MODE(p) ((p)->all.mode)
#define CFN_PARAM(p) ((p)->all.val)
#define CFN_RESET(p) ((p)->active=0, (p)->clear.val1=0, (p)->clear.val2=0)
#define CFN_GVAR_CST_MAX GVAR_LIMIT
#else
PACK(typedef struct t_CustomFnData {
PACK(union {
@ -948,6 +949,7 @@ PACK(typedef struct t_CustomFnData {
#define CFN_GVAR_MODE(p) ((p)->gvar.mode)
#define CFN_PARAM(p) ((p)->value)
#define CFN_RESET(p) ((p)->all.active = 0, CFN_PARAM(p) = 0)
#define CFN_GVAR_CST_MAX 125
#endif
enum TelemetryUnit {
@ -1244,7 +1246,7 @@ PACK(typedef struct t_SwashRingData { // Swash Ring data
#define NUM_ROTARY_ENCODERS_EXTRA 2
#define NUM_ROTARY_ENCODERS (2+NUM_ROTARY_ENCODERS_EXTRA)
#define ROTARY_ENCODER_ARRAY int16_t rotaryEncoders[2];
#define ROTARY_ENCODER_ARRAY_EXTRA int16_t rotaryEncodersExtra[MAX_PHASES][NUM_ROTARY_ENCODERS_EXTRA];
#define ROTARY_ENCODER_ARRAY_EXTRA int16_t rotaryEncodersExtra[MAX_FLIGHT_MODES][NUM_ROTARY_ENCODERS_EXTRA];
#elif defined(CPUM2560) && ROTARY_ENCODERS <= 2
#define NUM_ROTARY_ENCODERS_EXTRA 0
#define NUM_ROTARY_ENCODERS 2
@ -1369,8 +1371,8 @@ enum SwitchSources {
SWSRC_REb,
#endif
SWSRC_FIRST_CSW,
SWSRC_SW1 = SWSRC_FIRST_CSW,
SWSRC_FIRST_LOGICAL_SWITCH,
SWSRC_SW1 = SWSRC_FIRST_LOGICAL_SWITCH,
SWSRC_SW2,
SWSRC_SW3,
SWSRC_SW4,
@ -1382,13 +1384,24 @@ enum SwitchSources {
SWSRC_SWA,
SWSRC_SWB,
SWSRC_SWC,
SWSRC_LAST_CSW = SWSRC_SW1+NUM_LOGICAL_SWITCH-1,
SWSRC_LAST_LOGICAL_SWITCH = SWSRC_FIRST_LOGICAL_SWITCH+NUM_LOGICAL_SWITCH-1,
SWSRC_ON,
#if defined(CPUARM)
SWSRC_FIRST_FLIGHT_MODE,
SWSRC_LAST_FLIGHT_MODE = SWSRC_FIRST_FLIGHT_MODE+MAX_FLIGHT_MODES-1,
#endif
SWSRC_COUNT,
SWSRC_OFF = -SWSRC_ON,
SWSRC_FIRST = SWSRC_OFF,
SWSRC_LAST = SWSRC_ON
SWSRC_LAST = SWSRC_COUNT-1,
SWSRC_FIRST = -SWSRC_LAST,
SWSRC_LAST_SHORT_LIST = SWSRC_LAST_LOGICAL_SWITCH,
SWSRC_FIRST_SHORT_LIST = -SWSRC_LAST_SHORT_LIST,
};
enum MixSources {
@ -1680,7 +1693,7 @@ PACK(typedef struct t_ModelData {
LogicalSwitchData customSw[NUM_LOGICAL_SWITCH];
CustomFnData funcSw[NUM_CFN];
SwashRingData swashR;
PhaseData phaseData[MAX_PHASES];
PhaseData phaseData[MAX_FLIGHT_MODES];
AVR_FIELD(int8_t ppmFrameLength) // 0=22.5ms (10ms-30ms) 0.5ms increments
uint8_t thrTraceSrc;

139
radio/src/opentx.cpp
View file

@ -319,7 +319,8 @@ void per10ms()
if (lightOffCounter) lightOffCounter--;
if (flashCounter) flashCounter--;
if (s_noHi) s_noHi--;
if (trimsCheckTimer) trimsCheckTimer --;
if (trimsCheckTimer) trimsCheckTimer--;
if (ppmInValid) ppmInValid--;
#if defined(RTCLOCK)
/* Update global Date/Time every 100 per10ms cycles */
@ -768,7 +769,7 @@ int applyCurve(int x, CurveRef & curve)
switch (curve.type) {
case CURVE_REF_DIFF:
{
int curveParam = calc100to256(GET_GVAR(curve.value, -100, 100, s_perout_flight_phase));
int curveParam = calc100to256(GET_GVAR(curve.value, -100, 100, s_perout_flight_mode));
if (curveParam > 0 && x < 0)
x = (x * (256 - curveParam)) >> 8;
else if (curveParam < 0 && x > 0)
@ -777,7 +778,7 @@ int applyCurve(int x, CurveRef & curve)
}
case CURVE_REF_EXPO:
return expo(x, GET_GVAR(curve.value, -100, 100, s_perout_flight_phase));
return expo(x, GET_GVAR(curve.value, -100, 100, s_perout_flight_mode));
case CURVE_REF_FUNC:
switch (curve.value) {
@ -980,7 +981,7 @@ void applyExpos(int16_t *anas, uint8_t mode APPLY_EXPOS_EXTRA_PARAMS)
if (!EXPO_VALID(ed)) break; // end of list
if (ed->chn == cur_chn)
continue;
if (ed->phases & (1<<s_perout_flight_phase))
if (ed->phases & (1<<s_perout_flight_mode))
continue;
if (getSwitch(ed->swtch)) {
#if defined(PCBTARANIS)
@ -1019,18 +1020,18 @@ void applyExpos(int16_t *anas, uint8_t mode APPLY_EXPOS_EXTRA_PARAMS)
if (ed->curveMode == MODE_CURVE)
v = applyCurve(v, curveParam);
else
v = expo(v, GET_GVAR(curveParam, -100, 100, s_perout_flight_phase));
v = expo(v, GET_GVAR(curveParam, -100, 100, s_perout_flight_mode));
}
#endif
//========== WEIGHT ===============
int16_t weight = GET_GVAR(ed->weight, MIN_EXPO_WEIGHT, 100, s_perout_flight_phase);
int16_t weight = GET_GVAR(ed->weight, MIN_EXPO_WEIGHT, 100, s_perout_flight_mode);
weight = calc100to256(weight);
v = ((int32_t)v * weight) >> 8;
#if defined(PCBTARANIS)
//========== OFFSET ===============
int16_t offset = GET_GVAR(ed->offset, -100, 100, s_perout_flight_phase);
int16_t offset = GET_GVAR(ed->offset, -100, 100, s_perout_flight_mode);
if (offset) v += calc100toRESX(offset);
//========== TRIMS ================
@ -1267,7 +1268,7 @@ getvalue_t getValue(uint8_t i)
return 0;
#endif
else if (i<=MIXSRC_TrimAil) return calc1000toRESX((int16_t)8 * getTrimValue(s_perout_flight_phase, i-MIXSRC_TrimRud));
else if (i<=MIXSRC_TrimAil) return calc1000toRESX((int16_t)8 * getTrimValue(s_perout_flight_mode, i-MIXSRC_TrimRud));
#if defined(PCBTARANIS)
else if (i==MIXSRC_SA) return (switchState(SW_SA0) ? -1024 : (switchState(SW_SA1) ? 0 : 1024));
@ -1278,7 +1279,7 @@ getvalue_t getValue(uint8_t i)
else if (i==MIXSRC_SF) return (switchState(SW_SF0) ? -1024 : 1024);
else if (i==MIXSRC_SG) return (switchState(SW_SG0) ? -1024 : (switchState(SW_SG1) ? 0 : 1024));
else if (i==MIXSRC_SH) return (switchState(SW_SH0) ? -1024 : 1024);
else if (i<=MIXSRC_LAST_LOGICAL_SWITCH) return getSwitch(SWSRC_FIRST_CSW+i-MIXSRC_FIRST_LOGICAL_SWITCH) ? 1024 : -1024;
else if (i<=MIXSRC_LAST_LOGICAL_SWITCH) return getSwitch(SWSRC_FIRST_LOGICAL_SWITCH+i-MIXSRC_FIRST_LOGICAL_SWITCH) ? 1024 : -1024;
#else
else if (i==MIXSRC_3POS) return (getSwitch(SW_ID0-SW_BASE+1) ? -1024 : (getSwitch(SW_ID1-SW_BASE+1) ? 0 : 1024));
// don't use switchState directly to give getSwitch possibility to hack values if needed for switch warning
@ -1293,7 +1294,7 @@ getvalue_t getValue(uint8_t i)
else if (i<=MIXSRC_LAST_CH) return ex_chans[i-MIXSRC_CH1];
#if defined(GVARS)
else if (i<=MIXSRC_LAST_GVAR) return GVAR_VALUE(i-MIXSRC_GVAR1, getGVarFlightPhase(s_perout_flight_phase, i-MIXSRC_GVAR1));
else if (i<=MIXSRC_LAST_GVAR) return GVAR_VALUE(i-MIXSRC_GVAR1, getGVarFlightPhase(s_perout_flight_mode, i-MIXSRC_GVAR1));
#endif
else if (i==MIXSRC_FIRST_TELEM-1+TELEM_TX_VOLTAGE) return g_vbat100mV;
@ -1512,9 +1513,15 @@ bool getSwitch(int8_t swtch)
else if (cs_idx == SWSRC_REb) {
result = REB_DOWN();
}
#endif
#if defined(CPUARM) && defined(FLIGHT_MODES)
else if (cs_idx >= SWSRC_FIRST_FLIGHT_MODE) {
uint8_t idx = cs_idx - SWSRC_FIRST_FLIGHT_MODE;
result = (idx == s_perout_flight_mode);
}
#endif
else {
cs_idx -= SWSRC_FIRST_CSW;
cs_idx -= SWSRC_FIRST_LOGICAL_SWITCH;
GETSWITCH_RECURSIVE_TYPE mask = ((GETSWITCH_RECURSIVE_TYPE)1 << cs_idx);
if (s_last_switch_used & mask) {
@ -1800,7 +1807,7 @@ int8_t getMovedSource(GET_MOVED_SOURCE_PARAMS)
#if defined(FLIGHT_MODES)
uint8_t getFlightPhase()
{
for (uint8_t i=1; i<MAX_PHASES; i++) {
for (uint8_t i=1; i<MAX_FLIGHT_MODES; i++) {
PhaseData *phase = &g_model.phaseData[i];
if (phase->swtch && getSwitch(phase->swtch)) {
return i;
@ -1824,7 +1831,7 @@ int getTrimValue(uint8_t phase, uint8_t idx)
{
#if defined(PCBTARANIS)
int result = 0;
for (uint8_t i=0; i<MAX_PHASES; i++) {
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
trim_t v = getRawTrimValue(phase, idx);
if (v.mode == TRIM_MODE_NONE) {
return result;
@ -1851,7 +1858,7 @@ int getTrimValue(uint8_t phase, uint8_t idx)
void setTrimValue(uint8_t phase, uint8_t idx, int trim)
{
#if defined(PCBTARANIS)
for (uint8_t i=0; i<MAX_PHASES; i++) {
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
trim_t & v = phaseAddress(phase)->trim[idx];
if (v.mode == TRIM_MODE_NONE)
return;
@ -1883,7 +1890,7 @@ void setTrimValue(uint8_t phase, uint8_t idx, int trim)
#if !defined(PCBTARANIS)
uint8_t getTrimFlightPhase(uint8_t phase, uint8_t idx)
{
for (uint8_t i=0; i<MAX_PHASES; i++) {
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
if (phase == 0) return 0;
trim_t trim = getRawTrimValue(phase, idx);
if (trim <= TRIM_EXTENDED_MAX) return phase;
@ -1898,8 +1905,8 @@ uint8_t getTrimFlightPhase(uint8_t phase, uint8_t idx)
#if defined(ROTARY_ENCODERS)
uint8_t getRotaryEncoderFlightPhase(uint8_t idx)
{
uint8_t phase = s_perout_flight_phase;
for (uint8_t i=0; i<MAX_PHASES; i++) {
uint8_t phase = s_perout_flight_mode;
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
if (phase == 0) return 0;
#if ROTARY_ENCODERS > 2
int16_t value;
@ -1989,7 +1996,7 @@ uint8_t s_gvar_last = 0;
uint8_t getGVarFlightPhase(uint8_t phase, uint8_t idx)
{
for (uint8_t i=0; i<MAX_PHASES; i++) {
for (uint8_t i=0; i<MAX_FLIGHT_MODES; i++) {
if (phase == 0) return 0;
int16_t val = GVAR_VALUE(idx, phase); // TODO phase at the end everywhere to be consistent!
if (val <= GVAR_MAX) return phase;
@ -2144,7 +2151,7 @@ getvalue_t convert8bitsTelemValue(uint8_t channel, ls_telemetry_value_t value)
result = value * 5;
break;
case TELEM_CONSUMPTION:
result = value * 20;
result = value * 100;
break;
case TELEM_VSPEED:
result = ((getvalue_t)value - 125) * 10;
@ -2690,13 +2697,13 @@ uint8_t checkTrim(uint8_t event)
#if defined(PCBSTD)
phase = 0;
#else
phase = getGVarFlightPhase(s_perout_flight_phase, trimGvar[idx]);
phase = getGVarFlightPhase(s_perout_flight_mode, trimGvar[idx]);
#endif
before = GVAR_VALUE(trimGvar[idx], phase);
thro = false;
}
else {
phase = getTrimFlightPhase(s_perout_flight_phase, idx);
phase = getTrimFlightPhase(s_perout_flight_mode, idx);
#if defined(PCBTARANIS)
before = getTrimValue(phase, idx);
#else
@ -2705,7 +2712,7 @@ uint8_t checkTrim(uint8_t event)
thro = (idx==THR_STICK && g_model.thrTrim);
}
#else
phase = getTrimFlightPhase(s_perout_flight_phase, idx);
phase = getTrimFlightPhase(s_perout_flight_mode, idx);
#if defined(PCBTARANIS)
before = getTrimValue(phase, idx);
#else
@ -3080,7 +3087,7 @@ uint16_t isqrt32(uint32_t n)
FORCEINLINE void evalTrims()
{
uint8_t phase = s_perout_flight_phase;
uint8_t phase = s_perout_flight_mode;
for (uint8_t i=0; i<NUM_STICKS; i++) {
// do trim -> throttle trim if applicable
int16_t trim = getTrimValue(phase, i);
@ -3196,7 +3203,7 @@ void evalInputs(uint8_t mode)
}
#endif
if (mode <= e_perout_mode_inactive_phase && isFunctionActive(FUNCTION_TRAINER+ch)) {
if (mode <= e_perout_mode_inactive_phase && isFunctionActive(FUNCTION_TRAINER+ch) && ppmInValid) {
// trainer mode
TrainerMix* td = &g_eeGeneral.trainer.mix[ch];
if (td->mode) {
@ -3530,14 +3537,14 @@ void evalFunctions()
#if defined(GVARS)
case FUNC_ADJUST_GVAR:
if (CFN_GVAR_MODE(sd) == 0) {
SET_GVAR(CFN_GVAR_INDEX(sd), CFN_PARAM(sd), s_perout_flight_phase);
SET_GVAR(CFN_GVAR_INDEX(sd), CFN_PARAM(sd), s_perout_flight_mode);
}
else if (CFN_GVAR_MODE(sd) == 2) {
SET_GVAR(CFN_GVAR_INDEX(sd), GVAR_VALUE(CFN_PARAM(sd), s_perout_flight_phase), s_perout_flight_phase);
SET_GVAR(CFN_GVAR_INDEX(sd), GVAR_VALUE(CFN_PARAM(sd), s_perout_flight_mode), s_perout_flight_mode);
}
else if (CFN_GVAR_MODE(sd) == 3) {
if (!(activeFnSwitches & switch_mask)) {
SET_GVAR(CFN_GVAR_INDEX(sd), GVAR_VALUE(CFN_GVAR_INDEX(sd), getGVarFlightPhase(s_perout_flight_phase, CFN_GVAR_INDEX(sd))) + (CFN_PARAM(sd) ? +1 : -1), s_perout_flight_phase);
SET_GVAR(CFN_GVAR_INDEX(sd), GVAR_VALUE(CFN_GVAR_INDEX(sd), getGVarFlightPhase(s_perout_flight_mode, CFN_GVAR_INDEX(sd))) + (CFN_PARAM(sd) ? +1 : -1), s_perout_flight_mode);
}
}
else if (CFN_PARAM(sd) >= MIXSRC_TrimRud && CFN_PARAM(sd) <= MIXSRC_TrimAil) {
@ -3547,12 +3554,12 @@ void evalFunctions()
else if (CFN_PARAM(sd) >= MIXSRC_REa && CFN_PARAM(sd) < MIXSRC_TrimRud) {
int8_t scroll = rePreviousValues[CFN_PARAM(sd)-MIXSRC_REa] - (g_rotenc[CFN_PARAM(sd)-MIXSRC_REa] / ROTARY_ENCODER_GRANULARITY);
if (scroll) {
SET_GVAR(CFN_GVAR_INDEX(sd), GVAR_VALUE(CFN_GVAR_INDEX(sd), getGVarFlightPhase(s_perout_flight_phase, CFN_GVAR_INDEX(sd))) + scroll, s_perout_flight_phase);
SET_GVAR(CFN_GVAR_INDEX(sd), GVAR_VALUE(CFN_GVAR_INDEX(sd), getGVarFlightPhase(s_perout_flight_mode, CFN_GVAR_INDEX(sd))) + scroll, s_perout_flight_mode);
}
}
#endif
else {
SET_GVAR(CFN_GVAR_INDEX(sd), limit((getvalue_t)-LIMIT_EXT_MAX, getValue(CFN_PARAM(sd)), (getvalue_t)LIMIT_EXT_MAX) / 10, s_perout_flight_phase);
SET_GVAR(CFN_GVAR_INDEX(sd), limit((getvalue_t)-LIMIT_EXT_MAX, getValue(CFN_PARAM(sd)), (getvalue_t)LIMIT_EXT_MAX) / 10, s_perout_flight_mode);
}
break;
#endif
@ -3635,7 +3642,7 @@ void evalFunctions()
else {
#if defined(GVARS)
if (CFN_FUNC(sd) == FUNC_PLAY_TRACK && param > 250)
param = GVAR_VALUE(param-251, getGVarFlightPhase(s_perout_flight_phase, param-251));
param = GVAR_VALUE(param-251, getGVarFlightPhase(s_perout_flight_mode, param-251));
#endif
PUSH_CUSTOM_PROMPT(active ? param : param+1, i+1);
}
@ -3716,7 +3723,7 @@ void evalFunctions()
#define HELI_ANAS_ARRAY anas
#endif
uint8_t s_perout_flight_phase;
uint8_t s_perout_flight_mode;
void perOut(uint8_t mode, uint8_t tick10ms)
{
evalInputs(mode);
@ -3821,7 +3828,11 @@ void perOut(uint8_t mode, uint8_t tick10ms)
//========== PHASE && SWITCH =====
bool mixCondition = (md->phases != 0 || md->swtch);
delayval_t mixEnabled = !(md->phases & (1 << s_perout_flight_phase)) && getSwitch(md->swtch);
delayval_t mixEnabled = !(md->phases & (1 << s_perout_flight_mode)) && getSwitch(md->swtch);
if (mixEnabled && md->srcRaw >= MIXSRC_FIRST_TRAINER && md->srcRaw <= MIXSRC_LAST_TRAINER && !ppmInValid) {
mixEnabled = 0;
}
//========== VALUE ===============
getvalue_t v = 0;
@ -3906,14 +3917,14 @@ void perOut(uint8_t mode, uint8_t tick10ms)
if (apply_offset_and_curve) {
#if !defined(PCBTARANIS) // OFFSET is now applied AFTER weight on Taranis
//========== OFFSET / SOURCE ===============
int16_t offset = GET_GVAR(MD_OFFSET(md), GV_RANGELARGE_NEG, GV_RANGELARGE, s_perout_flight_phase);
int16_t offset = GET_GVAR(MD_OFFSET(md), GV_RANGELARGE_NEG, GV_RANGELARGE, s_perout_flight_mode);
if (offset) v += calc100toRESX_16Bits(offset);
#endif
//========== TRIMS ================
if (!(mode & e_perout_mode_notrims)) {
#if defined(PCBTARANIS)
if (!md->carryTrim) {
if (md->carryTrim == 0) {
int8_t mix_trim;
if (stickIndex < NUM_STICKS)
mix_trim = stickIndex;
@ -3921,7 +3932,13 @@ void perOut(uint8_t mode, uint8_t tick10ms)
mix_trim = virtualInputsTrims[md->srcRaw-1];
else
mix_trim = -1;
if (mix_trim >= 0) v += trims[mix_trim];
if (mix_trim >= 0) {
int16_t trim = trims[mix_trim];
if (mix_trim == THR_STICK && g_model.throttleReversed)
v -= trim;
else
v += trim;
}
}
#else
int8_t mix_trim = md->carryTrim;
@ -3931,13 +3948,19 @@ void perOut(uint8_t mode, uint8_t tick10ms)
mix_trim = stickIndex;
else
mix_trim = -1;
if (mix_trim >= 0) v += trims[mix_trim];
if (mix_trim >= 0) {
int16_t trim = trims[mix_trim];
if (mix_trim == THR_STICK && g_model.throttleReversed)
v -= trim;
else
v += trim;
}
#endif
}
}
// saves 12 bytes code if done here and not together with weight; unknown reason
int16_t weight = GET_GVAR(MD_WEIGHT(md), GV_RANGELARGE_NEG, GV_RANGELARGE, s_perout_flight_phase);
int16_t weight = GET_GVAR(MD_WEIGHT(md), GV_RANGELARGE_NEG, GV_RANGELARGE, s_perout_flight_mode);
weight = calc100to256_16Bits(weight);
//========== SPEED ===============
@ -3998,7 +4021,7 @@ void perOut(uint8_t mode, uint8_t tick10ms)
//========== OFFSET / AFTER ===============
#if defined(PCBTARANIS)
if (apply_offset_and_curve) {
int16_t offset = GET_GVAR(MD_OFFSET(md), GV_RANGELARGE_NEG, GV_RANGELARGE, s_perout_flight_phase);
int16_t offset = GET_GVAR(MD_OFFSET(md), GV_RANGELARGE_NEG, GV_RANGELARGE, s_perout_flight_mode);
if (offset) dv += calc100toRESX_16Bits(offset) << 8;
}
#endif
@ -4011,7 +4034,7 @@ void perOut(uint8_t mode, uint8_t tick10ms)
#else
if (md->curveMode == MODE_DIFFERENTIAL) {
// @@@2 also recalculate curveParam to a 256 basis which ease the calculation later a lot
int16_t curveParam = calc100to256(GET_GVAR(md->curveParam, -100, 100, s_perout_flight_phase));
int16_t curveParam = calc100to256(GET_GVAR(md->curveParam, -100, 100, s_perout_flight_mode));
if (curveParam > 0 && dv < 0)
dv = (dv * (256 - curveParam)) >> 8;
else if (curveParam < 0 && dv > 0)
@ -4140,7 +4163,7 @@ void doMixerCalculations()
#endif
#define MAX_ACT 0xffff
static uint16_t fp_act[MAX_PHASES] = {0};
static uint16_t fp_act[MAX_FLIGHT_MODES] = {0};
static uint16_t delta = 0;
static ACTIVE_PHASES_TYPE s_fade_flight_phases = 0;
static uint8_t s_last_phase = 255; // TODO reinit everything here when the model changes, no???
@ -4175,10 +4198,10 @@ void doMixerCalculations()
int32_t weight = 0;
if (s_fade_flight_phases) {
memclear(sum_chans512, sizeof(sum_chans512));
for (uint8_t p=0; p<MAX_PHASES; p++) {
for (uint8_t p=0; p<MAX_FLIGHT_MODES; p++) {
s_last_switch_used = 0;
if (s_fade_flight_phases & ((ACTIVE_PHASES_TYPE)1 << p)) {
s_perout_flight_phase = p;
s_perout_flight_mode = p;
perOut(p==phase ? e_perout_mode_normal : e_perout_mode_inactive_phase, p==phase ? tick10ms : 0);
for (uint8_t i=0; i<NUM_CHNOUT; i++)
sum_chans512[i] += (chans[i] >> 4) * fp_act[p];
@ -4187,10 +4210,10 @@ void doMixerCalculations()
s_last_switch_used = 0;
}
assert(weight);
s_perout_flight_phase = phase;
s_perout_flight_mode = phase;
}
else {
s_perout_flight_phase = phase;
s_perout_flight_mode = phase;
perOut(e_perout_mode_normal, tick10ms);
}
@ -4522,7 +4545,7 @@ void doMixerCalculations()
if (s_fade_flight_phases) {
uint16_t tick_delta = delta * tick10ms;
for (uint8_t p=0; p<MAX_PHASES; p++) {
for (uint8_t p=0; p<MAX_FLIGHT_MODES; p++) {
ACTIVE_PHASES_TYPE phaseMask = ((ACTIVE_PHASES_TYPE)1 << p);
if (s_fade_flight_phases & phaseMask) {
if (p == phase) {
@ -5046,6 +5069,7 @@ void perMain()
int16_t g_ppmIns[NUM_TRAINER];
uint8_t ppmInState = 0; // 0=unsync 1..8= wait for value i-1
uint8_t ppmInValid = 0;
#if !defined(SIMU) && !defined(CPUARM)
@ -5132,21 +5156,20 @@ ISR(TIMER3_CAPT_vect) // G: High frequency noise can cause stack overflo with IS
// G: We process g_ppmIns immediately here, to make servo movement as smooth as possible
// while under trainee control
if (val>4000 && val < 16000) // G: Prioritize reset pulse. (Needed when less than 8 incoming pulses)
if (val>4000 && val < 16000) { // G: Prioritize reset pulse. (Needed when less than 8 incoming pulses)
ppmInState = 1; // triggered
else
{
if (ppmInState && ppmInState<=8)
{
if (val>800 && val<2200) // if valid pulse-width range
{
g_ppmIns[ppmInState++ - 1] =
(int16_t)(val - 1500)*(g_eeGeneral.PPM_Multiplier+10)/10; //+-500 != 512, but close enough.
}
else
else {
if (ppmInState>0 && ppmInState<=8) {
if (val>800 && val<2200) { // if valid pulse-width range
ppmInValid = 100;
g_ppmIns[ppmInState++ - 1] = (int16_t)(val - 1500) * (uint8_t)(g_eeGeneral.PPM_Multiplier+10)/10; //+-500 != 512, but close enough.
}
else {
ppmInState = 0; // not triggered
}
}
}
lastCapt = capture;
@ -5215,7 +5238,7 @@ void instantTrim()
for (uint8_t i=0; i<NUM_STICKS; i++) {
if (i!=THR_STICK) {
// don't instant trim the throttle stick
uint8_t trim_phase = getTrimFlightPhase(s_perout_flight_phase, i);
uint8_t trim_phase = getTrimFlightPhase(s_perout_flight_mode, i);
#if defined(PCBTARANIS)
int16_t trim = limit<int16_t>(TRIM_EXTENDED_MIN, (calibratedStick[i] + trims[i]) / 2, TRIM_EXTENDED_MAX);
#else
@ -5279,8 +5302,8 @@ void moveTrimsToOffsets() // copy state of 3 primary to subtrim
// reset all trims, except throttle (if throttle trim)
for (uint8_t i=0; i<NUM_STICKS; i++) {
if (i!=THR_STICK || !g_model.thrTrim) {
int16_t original_trim = getTrimValue(s_perout_flight_phase, i);
for (uint8_t phase=0; phase<MAX_PHASES; phase++) {
int16_t original_trim = getTrimValue(s_perout_flight_mode, i);
for (uint8_t phase=0; phase<MAX_FLIGHT_MODES; phase++) {
#if defined(PCBTARANIS)
trim_t trim = getRawTrimValue(phase, i);
if (trim.mode / 2 == phase)

3
radio/src/opentx.h
View file

@ -647,7 +647,7 @@ enum StartupWarningStates {
#define FORCE_INDIRECT(ptr) __asm__ __volatile__ ("" : "=e" (ptr) : "0" (ptr))
#endif
extern uint8_t s_perout_flight_phase;
extern uint8_t s_perout_flight_mode;
#if defined(CPUARM)
#define bitfield_channels_t uint32_t
@ -1013,6 +1013,7 @@ extern uint8_t g_beepCnt;
extern uint8_t g_beepVal[5];
extern uint8_t ppmInState; //0=unsync 1..8= wait for value i-1
extern uint8_t ppmInValid;
extern int16_t g_ppmIns[NUM_TRAINER];
extern int32_t chans[NUM_CHNOUT];
extern int16_t ex_chans[NUM_CHNOUT]; // Outputs (before LIMITS) of the last perMain

13
radio/src/targets/sky9x/board_sky9x.cpp
View file

@ -314,17 +314,16 @@ extern "C" void TC3_IRQHandler() //capture ppm in at 2MHz
ppmInState = 1; // triggered
}
else {
if (ppmInState && ppmInState<=16)
{
if (val>800 && val<2200) // if valid pulse-width range
{
g_ppmIns[ppmInState++ - 1] =
(int16_t)(val - 1500)*(g_eeGeneral.PPM_Multiplier+10)/10; //+-500 != 512, but close enough.
if (ppmInState>0 && ppmInState<=16) {
if (val>800 && val<2200) { // if valid pulse-width range
ppmInValid = 100;
g_ppmIns[ppmInState++ - 1] = (int16_t)(val - 1500)*(g_eeGeneral.PPM_Multiplier+10)/10; //+-500 != 512, but close enough.
}
else
else {
ppmInState = 0; // not triggered
}
}
}
lastCapt = capture;
}

7
radio/src/targets/taranis/trainer_driver.cpp
View file

@ -126,12 +126,13 @@ extern "C" void TIM3_IRQHandler()
// We process g_ppmInsright here to make servo movement as smooth as possible
// while under trainee control
if ((val>4000) && (val < 19000)) { // G: Prioritize reset pulse. (Needed when less than 16 incoming pulses)
if (val>4000 && val<19000) { // G: Prioritize reset pulse. (Needed when less than 16 incoming pulses)
ppmInState = 1; // triggered
}
else {
if (ppmInState && (ppmInState<=16)) {
if ((val>800) && (val<2200)) {
if (ppmInState>0 && ppmInState<=16) {
if (val>800 && val<2200) {
ppmInValid = 100;
g_ppmIns[ppmInState++ - 1] = (int16_t)(val - 1500)*(g_eeGeneral.PPM_Multiplier+10)/10; //+-500 != 512, but close enough.
}
else {

14
radio/src/translations/se.h.txt
View file

@ -294,9 +294,13 @@
#define TR_A3_A4_MIN
#endif
#define TR_ASPD_MAX "ASp+"
#define TR_ASPD_MAX TR("ASp+", "ASpd+")
#define TR_VTELEMCHNS "---\0""Batt""Tmr1""Tmr2" TR_SWR "Tx\0 ""Rx\0 " TR_RX_BATT "A1\0 ""A2\0 " TR_A3_A4 "Höjd""Varv""Tank""T1\0 ""T2\0 ""Fart""Avst""GHjd""Batt""Cels""Vfas""Curr""Cnsp""Powr""AccX""AccY""AccZ""Hdg\0""VFrt""ASpd""dTE\0" TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE "A1-\0""A2-\0" TR_A3_A4_MIN "Hjd-""Hjd+""Rpm+""T1+\0""T2+\0""Frt+""Avs+" TR_ASPD_MAX "Cel-""Cls-""Vfs-""Cur+""Pwr+" TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE "Acc\0""Tid\0"
#if LCD_W >= 212
#define TR_VTELEMCHNS "---\0 ""Batt\0""Tmr1\0""Tmr2\0" TR_SWR "Tx\0 ""Rx\0 " TR_RX_BATT "A1\0 ""A2\0 " TR_A3_A4 "Alt\0 ""Rpm\0 ""Fuel\0""T1\0 ""T2\0 ""Spd\0 ""Dist\0""GAlt\0""Cell\0""Cells""Vfas\0""Curr\0""Cnsp\0""Powr\0""AccX\0""AccY\0""AccZ\0""Hdg\0 ""VSpd\0""ASpd\0""dTE\0 " TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE "A1-\0 ""A2-\0 " TR_A3_A4_MIN "Alt-\0""Alt+\0""Rpm+\0""T1+\0 ""T2+\0 ""Spd+\0""Dst+\0" TR_ASPD_MAX "Cell-""Cels-""Vfas-""Curr+""Powr+" TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE "Acc\0 ""Time\0"
#else
#define TR_VTELEMCHNS "---\0""Batt""Tmr1""Tmr2" TR_SWR "Tx\0 ""Rx\0 " TR_RX_BATT "A1\0 ""A2\0 " TR_A3_A4 "Alt\0""Rpm\0""Fuel""T1\0 ""T2\0 ""Spd\0""Dist""GAlt""Cell""Cels""Vfas""Curr""Cnsp""Powr""AccX""AccY""AccZ""Hdg\0""VSpd""ASpd""dTE\0" TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE "A1-\0""A2-\0" TR_A3_A4_MIN "Alt-""Alt+""Rpm+""T1+\0""T2+\0""Spd+""Dst+" TR_ASPD_MAX "Cel-""Cls-""Vfs-""Cur+""Pwr+" TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE TR_TELEM_RESERVE "Acc\0""Time"
#endif
#define LENGTH_UNIT_IMP "ft\0"
#define SPEED_UNIT_IMP "mph"
@ -415,7 +419,7 @@
#define TR_CYC_VSRCRAW "[C1]""[C2]""[C3]"
#endif
#define TR_VSRCRAW "---\0""Rod\0""Hjd\0""Gas\0""Ske\0" TR_POTS_VSRCRAW TR_ROTARY_ENCODER "MAX " TR_CYC_VSRCRAW "TrmR" "TrmH" "TrmG" "TrmS" TR_SW_VSRCRAW
#define TR_VSRCRAW "---\0""Rod\0""Hjd\0""Gas\0""Ske\0" TR_POTS_VSRCRAW TR_ROTARY_ENCODERS "MAX\0" TR_CYC_VSRCRAW "TrmR" "TrmH" "TrmG" "TrmS" TR_SW_VSRCRAW
#define LEN_VTMRMODES "\003"
#define TR_VTMRMODES "Av\0""ABS""GAs""GA%""GAt"
@ -440,7 +444,6 @@
#define LEN_INDENT 1
#define INDENT_WIDTH (FW/2)
#if defined(PCBTARANIS)
#define TR_ENTER "[ENTER]"
#else
@ -475,7 +478,7 @@
#define TR_TTRIM TR("Gastrim", INDENT "Gastrim")
#define TR_BEEPCTR TR("Cent.pip", "Centerpip")
#define TR_PROTO TR(INDENT "Proto", INDENT "Protokoll")
#define TR_PPMFRAME "PPM-paket"
#define TR_PPMFRAME TR(INDENT "PPM-paket", INDENT "PPM-paket")
#define TR_MS "ms"
#define TR_SWITCH "Brytare"
#define TR_TRIMS "Trimmar"
@ -851,7 +854,6 @@
#define TR_ABOUT_HARDWARE_3 ""
#endif
#define TR_ABOUT_PARENTS_1 "Ursprungsprojekt"
#define TR_ABOUT_PARENTS_2 "ersky9x (Mike Blandford)"
#define TR_ABOUT_PARENTS_3 "ER9X (Erez Raviv)"