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Use std abs() instead of ABS() macro
Changes uses of ABS() macro to <stdlib.h> abs() and <math.h> fabsf()
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18 changed files with 43 additions and 30 deletions
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@ -20,6 +20,7 @@
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#include <stdbool.h>
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#include <stdint.h>
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#include <stdlib.h>
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#include <string.h>
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#include <math.h>
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@ -373,7 +374,7 @@ STATIC_UNIT_TESTED FAST_CODE_NOINLINE float calcHorizonLevelStrength()
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float horizonLevelStrength = 1.0f - MAX(fabsf(getLevelModeRcDeflection(FD_ROLL)), fabsf(getLevelModeRcDeflection(FD_PITCH)));
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// 0 at level, 90 at vertical, 180 at inverted (degrees):
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const float currentInclination = MAX(ABS(attitude.values.roll), ABS(attitude.values.pitch)) / 10.0f;
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const float currentInclination = MAX(abs(attitude.values.roll), abs(attitude.values.pitch)) / 10.0f;
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// horizonTiltExpertMode: 0 = leveling always active when sticks centered,
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// 1 = leveling can be totally off when inverted
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@ -480,8 +481,8 @@ static void handleCrashRecovery(
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&& fabsf(gyro.gyroADCf[FD_YAW]) < pidRuntime.crashRecoveryRate)) {
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if (sensors(SENSOR_ACC)) {
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// check aircraft nearly level
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if (ABS(attitude.raw[FD_ROLL] - angleTrim->raw[FD_ROLL]) < pidRuntime.crashRecoveryAngleDeciDegrees
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&& ABS(attitude.raw[FD_PITCH] - angleTrim->raw[FD_PITCH]) < pidRuntime.crashRecoveryAngleDeciDegrees) {
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if (abs(attitude.raw[FD_ROLL] - angleTrim->raw[FD_ROLL]) < pidRuntime.crashRecoveryAngleDeciDegrees
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&& abs(attitude.raw[FD_PITCH] - angleTrim->raw[FD_PITCH]) < pidRuntime.crashRecoveryAngleDeciDegrees) {
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pidRuntime.inCrashRecoveryMode = false;
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BEEP_OFF;
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}
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