1
0
Fork 0
mirror of https://github.com/betaflight/betaflight.git synced 2025-07-18 13:55:18 +03:00

AIR MODE Safety Enhancements

This commit is contained in:
borisbstyle 2015-12-08 00:22:49 +01:00
parent 72e9a4dc17
commit b84e9f4676
5 changed files with 46 additions and 18 deletions

View file

@ -61,8 +61,6 @@ uint8_t dynP8[3], dynI8[3], dynD8[3], PIDweight[3];
static int32_t errorGyroI[3] = { 0, 0, 0 };
static float errorGyroIf[3] = { 0.0f, 0.0f, 0.0f };
static int32_t errorAngleI[2] = { 0, 0 };
static float errorAngleIf[2] = { 0.0f, 0.0f };
static void pidRewrite(pidProfile_t *pidProfile, controlRateConfig_t *controlRateConfig,
uint16_t max_angle_inclination, rollAndPitchTrims_t *angleTrim, rxConfig_t *rxConfig);
@ -72,15 +70,6 @@ typedef void (*pidControllerFuncPtr)(pidProfile_t *pidProfile, controlRateConfig
pidControllerFuncPtr pid_controller = pidRewrite; // which pid controller are we using, defaultMultiWii
void pidResetErrorAngle(void)
{
errorAngleI[ROLL] = 0;
errorAngleI[PITCH] = 0;
errorAngleIf[ROLL] = 0.0f;
errorAngleIf[PITCH] = 0.0f;
}
void pidResetErrorGyro(void)
{
errorGyroI[ROLL] = 0;

View file

@ -75,6 +75,5 @@ extern int16_t axisPID[XYZ_AXIS_COUNT];
extern int32_t axisPID_P[3], axisPID_I[3], axisPID_D[3];
void pidSetController(pidControllerType_e type);
void pidResetErrorAngle(void);
void pidResetErrorGyro(void);

View file

@ -65,6 +65,7 @@ static pidProfile_t *pidProfile;
// true if arming is done via the sticks (as opposed to a switch)
static bool isUsingSticksToArm = true;
static bool rollPitchCentered = true; // Roll and pitch are centered, AIR Mode condition
int16_t rcCommand[4]; // interval [1000;2000] for THROTTLE and [-500;+500] for ROLL/PITCH/YAW
@ -106,6 +107,10 @@ bool isUsingSticksForArming(void)
return isUsingSticksToArm;
}
bool isRollPitchCentered(void)
{
return rollPitchCentered;
}
bool areSticksInApModePosition(uint16_t ap_mode)
{
@ -146,6 +151,12 @@ void processRcStickPositions(rxConfig_t *rxConfig, throttleStatus_e throttleStat
rcDelayCommand = 0;
rcSticks = stTmp;
if (rcSticks == PIT_CE + ROL_CE) {
rollPitchCentered = true;
} else {
rollPitchCentered = false;
}
// perform actions
if (!isUsingSticksToArm) {

View file

@ -126,7 +126,6 @@ typedef struct modeActivationCondition_s {
#define IS_RANGE_USABLE(range) ((range)->startStep < (range)->endStep)
#define SHOULD_RESET_ERRORS ((throttleStatus == THROTTLE_LOW && !(IS_RC_MODE_ACTIVE(BOXAIRMODE))) || !(ARMING_FLAG(ARMED)) || ((throttleStatus == THROTTLE_LOW && feature(FEATURE_MOTOR_STOP))))
typedef struct controlRateConfig_s {
uint8_t rcRate8;
uint8_t rcExpo8;
@ -244,3 +243,4 @@ bool isUsingSticksForArming(void);
int32_t getRcStickDeflection(int32_t axis, uint16_t midrc);
bool isModeActivationConditionPresent(modeActivationCondition_t *modeActivationConditions, boxId_e modeId);
bool isRollPitchCentered(void);

View file

@ -101,6 +101,10 @@ enum {
#define PREVENT_BARO_READ_PRE_LOOP_TRIGGER 150 // Prevent BARO processing before expected loop trigger
#define GYRO_RATE 0.001f // Gyro refresh rate 1khz
// AIR MODE Reset timers
#define ERROR_RESET_DEACTIVATE_DELAY (1 * 1000) // 1 sec delay to disable AIR MODE Iterm resetting
#define ERROR_RESET_ACTIVATE_DELAY (5 * 1000) // 5 sec delay to enable AIR MODE Iterm resetting
uint32_t currentTime = 0;
uint32_t previousTime = 0;
uint16_t cycleTime = 0; // this is the number in micro second to achieve a full loop, it can differ a little and is taken into account in the PID loop
@ -565,9 +569,36 @@ void processRx(void)
throttleStatus_e throttleStatus = calculateThrottleStatus(&masterConfig.rxConfig, masterConfig.flight3DConfig.deadband3d_throttle);
if (SHOULD_RESET_ERRORS) {
pidResetErrorAngle();
static bool airModeErrorResetIsEnabled = true; // Should always initialize with reset enabled
static uint32_t airModeErrorResetToggleTimeout = 0; // Timeout for both activate and deactivate mode
if (throttleStatus == THROTTLE_LOW) {
// Evaluate if the error needs resetting again. Should be entered when in air mode during landings etc...
if ((IS_RC_MODE_ACTIVE(BOXAIRMODE)) && !airModeErrorResetIsEnabled) {
if ((millis() > airModeErrorResetToggleTimeout) && isRollPitchCentered()) {
airModeErrorResetIsEnabled = true;
}
}
// Conditions to reset Error
if (!IS_RC_MODE_ACTIVE(BOXARM) || feature(FEATURE_MOTOR_STOP) || ((IS_RC_MODE_ACTIVE(BOXAIRMODE)) && airModeErrorResetIsEnabled)) {
pidResetErrorGyro();
airModeErrorResetToggleTimeout = millis() + ERROR_RESET_DEACTIVATE_DELAY; // Reset de-activate timer
}
} else {
if (!(feature(FEATURE_MOTOR_STOP)) && IS_RC_MODE_ACTIVE(BOXARM) && IS_RC_MODE_ACTIVE(BOXAIRMODE)) {
if (airModeErrorResetIsEnabled) {
if ((millis() > airModeErrorResetToggleTimeout) && !isRollPitchCentered()) { // Only disable error reset when roll and pitch not centered
airModeErrorResetIsEnabled = false;
airModeErrorResetToggleTimeout = millis() + ERROR_RESET_ACTIVATE_DELAY; // Start reset activate timer
}
} else if (!airModeErrorResetIsEnabled) {
airModeErrorResetToggleTimeout = millis() + ERROR_RESET_ACTIVATE_DELAY; // Reset activate timer
}
} else {
airModeErrorResetIsEnabled = true; // This is needed to reset procedure when switch is toggled in air
}
}
// When armed and motors aren't spinning, do beeps and then disarm
@ -634,7 +665,6 @@ void processRx(void)
canUseHorizonMode = false;
if (!FLIGHT_MODE(ANGLE_MODE)) {
pidResetErrorAngle();
ENABLE_FLIGHT_MODE(ANGLE_MODE);
}
} else {
@ -646,7 +676,6 @@ void processRx(void)
DISABLE_FLIGHT_MODE(ANGLE_MODE);
if (!FLIGHT_MODE(HORIZON_MODE)) {
pidResetErrorAngle();
ENABLE_FLIGHT_MODE(HORIZON_MODE);
}
} else {