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Rename a few more flags

NAV -> USE_NAV
FIXED_WING_LANDING -> NAV_FIXED_WING_LANDING
ASYNC_GYRO_PROCESSING -> USE_ASYNC_GYRO_PROCESSING
BOOTLOG -> USE_BOOTLOG
STATS -> USE_STATS
This commit is contained in:
Alberto García Hierro 2017-12-04 12:58:51 +00:00
parent 7a1491e158
commit d5ba9c4eec
38 changed files with 112 additions and 112 deletions

View file

@ -21,7 +21,7 @@
#include "platform.h"
#if defined(NAV)
#if defined(USE_NAV)
#include "build/build_config.h"
#include "build/debug.h"
@ -428,7 +428,7 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
pitchCorrection += posControl.rcAdjustment[PITCH];
throttleCorrection += DECIDEGREES_TO_DEGREES(pitchCorrection) * navConfig()->fw.pitch_to_throttle;
#ifdef FIXED_WING_LANDING
#ifdef NAV_FIXED_WING_LANDING
if (navStateFlags & NAV_CTL_LAND) {
/*
* During LAND we do not allow to raise THROTTLE when nose is up
@ -438,7 +438,7 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
} else {
#endif
throttleCorrection = constrain(throttleCorrection, minThrottleCorrection, maxThrottleCorrection);
#ifdef FIXED_WING_LANDING
#ifdef NAV_FIXED_WING_LANDING
}
#endif
}
@ -467,7 +467,7 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
rcCommand[THROTTLE] = constrain(correctedThrottleValue, motorConfig()->minthrottle, motorConfig()->maxthrottle);
}
#ifdef FIXED_WING_LANDING
#ifdef NAV_FIXED_WING_LANDING
/*
* Then altitude is below landing slowdown min. altitude, enable final approach procedure
* TODO refactor conditions in this metod if logic is proven to be correct