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[RTH] minor readability improvements

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This commit is contained in:
Michel Pastor 2019-06-04 04:15:05 +02:00
parent 19faf75e75
commit d23c161e59
1 changed files with 12 additions and 13 deletions
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25
src/main/navigation/navigation.c
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@ -1113,11 +1113,12 @@ static navigationFSMEvent_t navOnEnteringState_NAV_STATE_RTH_CLIMB_TO_SAFE_ALT(n
// If we have valid pos sensor OR we are configured to ignore GPS loss
if ((posControl.flags.estPosStatus >= EST_USABLE) || !checkForPositionSensorTimeout() || navConfig()->general.flags.rth_climb_ignore_emerg) {
const float rthAltitudeMargin = STATE(FIXED_WING) ?
MAX(FW_RTH_CLIMB_MARGIN_MIN_CM, (FW_RTH_CLIMB_MARGIN_PERCENT/100.0) * fabsf(posControl.rthState.rthInitialAltitude - posControl.rthState.homePosition.pos.z)) : // Airplane
MAX(MR_RTH_CLIMB_MARGIN_MIN_CM, (MR_RTH_CLIMB_MARGIN_PERCENT/100.0) * fabsf(posControl.rthState.rthInitialAltitude - posControl.rthState.homePosition.pos.z)); // Copters
const uint8_t rthClimbMarginPercent = STATE(FIXED_WING) ? FW_RTH_CLIMB_MARGIN_PERCENT : MR_RTH_CLIMB_MARGIN_PERCENT;
const float rthAltitudeMargin = MAX(FW_RTH_CLIMB_MARGIN_MIN_CM, (rthClimbMarginPercent/100.0) * fabsf(posControl.rthState.rthInitialAltitude - posControl.rthState.homePosition.pos.z));
// If we reached desired initial RTH altitude or we don't want to climb first
if (((navGetCurrentActualPositionAndVelocity()->pos.z - posControl.rthState.rthInitialAltitude) > -rthAltitudeMargin) || (!navConfig()->general.flags.rth_climb_first)) {
// Delayed initialization for RTH sanity check on airplanes - allow to finish climb first as it can take some distance
if (STATE(FIXED_WING)) {
initializeRTHSanityChecker(&navGetCurrentActualPositionAndVelocity()->pos);
@ -1135,23 +1136,21 @@ static navigationFSMEvent_t navOnEnteringState_NAV_STATE_RTH_CLIMB_TO_SAFE_ALT(n
}
return NAV_FSM_EVENT_SUCCESS; // NAV_STATE_RTH_HEAD_HOME
}
else {
} else {
fpVector3_t * tmpHomePos = rthGetHomeTargetPosition(RTH_HOME_ENROUTE_INITIAL);
/* For multi-rotors execute sanity check during initial ascent as well */
if (!STATE(FIXED_WING)) {
if (!validateRTHSanityChecker()) {
return NAV_FSM_EVENT_SWITCH_TO_EMERGENCY_LANDING;
}
if (!STATE(FIXED_WING) && !validateRTHSanityChecker()) {
return NAV_FSM_EVENT_SWITCH_TO_EMERGENCY_LANDING;
}
// Climb to safe altitude and turn to correct direction
if (STATE(FIXED_WING)) {
tmpHomePos->z += FW_RTH_CLIMB_OVERSHOOT_CM;
setDesiredPosition(tmpHomePos, 0, NAV_POS_UPDATE_Z);
}
else {
} else {
// Until the initial climb phase is complete target slightly *above* the cruise altitude to ensure we actually reach
// it in a reasonable time. Immediately after we finish this phase - target the original altitude.
tmpHomePos->z += MR_RTH_CLIMB_OVERSHOOT_CM;
@ -1164,6 +1163,7 @@ static navigationFSMEvent_t navOnEnteringState_NAV_STATE_RTH_CLIMB_TO_SAFE_ALT(n
}
return NAV_FSM_EVENT_NONE;
}
}
/* Position sensor failure timeout - land */
@ -2109,8 +2109,7 @@ static void updateDesiredRTHAltitude(void)
posControl.rthState.rthFinalAltitude = posControl.rthState.homePosition.pos.z + navConfig()->general.rth_altitude;
}
}
}
else {
} else {
posControl.rthState.rthInitialAltitude = posControl.actualState.abs.pos.z;
posControl.rthState.rthFinalAltitude = posControl.actualState.abs.pos.z;
}