1
0
Fork 0
mirror of https://github.com/betaflight/betaflight.git synced 2025-07-26 01:35:41 +03:00
This commit is contained in:
treymarc 2014-04-12 02:51:42 +00:00
parent aa253a387d
commit cabf7eaac3
7 changed files with 25 additions and 26 deletions

View file

@ -51,11 +51,11 @@ uint16_t GPS_ground_course = 0; // degrees * 10
int16_t nav[2];
int16_t nav_rated[2]; // Adding a rate controller to the navigation to make it smoother
int8_t nav_mode = NAV_MODE_NONE; // Navigation mode
uint8_t GPS_numCh; // Number of channels
uint8_t GPS_svinfo_chn[16]; // Channel number
uint8_t GPS_svinfo_svid[16]; // Satellite ID
uint8_t GPS_svinfo_quality[16]; // Bitfield Qualtity
uint8_t GPS_svinfo_cno[16]; // Carrier to Noise Ratio (Signal Strength)
uint8_t GPS_numCh; // Number of channels
uint8_t GPS_svinfo_chn[16]; // Channel number
uint8_t GPS_svinfo_svid[16]; // Satellite ID
uint8_t GPS_svinfo_quality[16]; // Bitfield Qualtity
uint8_t GPS_svinfo_cno[16]; // Carrier to Noise Ratio (Signal Strength)
// Automatic ACC Offset Calibration
uint16_t InflightcalibratingA = 0;
@ -103,7 +103,7 @@ void annexCode(void)
prop2 = 100;
} else {
if (rcData[THROTTLE] < 2000) {
prop2 = 100 - (uint16_t) cfg.dynThrPID * (rcData[THROTTLE] - cfg.tpaBreakPoint) / (2000 - cfg.tpaBreakPoint);
prop2 = 100 - (uint16_t)cfg.dynThrPID * (rcData[THROTTLE] - cfg.tpaBreakPoint) / (2000 - cfg.tpaBreakPoint);
} else {
prop2 = 100 - cfg.dynThrPID;
}
@ -143,7 +143,7 @@ void annexCode(void)
}
tmp = constrain(rcData[THROTTLE], mcfg.mincheck, 2000);
tmp = (uint32_t) (tmp - mcfg.mincheck) * 1000 / (2000 - mcfg.mincheck); // [MINCHECK;2000] -> [0;1000]
tmp = (uint32_t)(tmp - mcfg.mincheck) * 1000 / (2000 - mcfg.mincheck); // [MINCHECK;2000] -> [0;1000]
tmp2 = tmp / 100;
rcCommand[THROTTLE] = lookupThrottleRC[tmp2] + (tmp - tmp2 * 100) * (lookupThrottleRC[tmp2 + 1] - lookupThrottleRC[tmp2]) / 100; // [0;1000] -> expo -> [MINTHROTTLE;MAXTHROTTLE]
@ -363,7 +363,7 @@ static void pidRewrite(void)
// ----------PID controller----------
for (axis = 0; axis < 3; axis++) {
// -----Get the desired angle rate depending on flight mode
if ((f.ANGLE_MODE || f.HORIZON_MODE) && axis < 2 ) { // MODE relying on ACC
if ((f.ANGLE_MODE || f.HORIZON_MODE) && axis < 2) { // MODE relying on ACC
// calculate error and limit the angle to max configured inclination
errorAngle = constrain((rcCommand[axis] << 1) + GPS_angle[axis], -((int)mcfg.max_angle_inclination), +mcfg.max_angle_inclination) - angle[axis] + cfg.angleTrim[axis]; // 16 bits is ok here
}