moved flipOverAfterPowerFactor in motorConfig

src/main/fc/controlrate_profile.c

@@ -65,7 +65,6 @@ void pgResetFn_controlRateProfiles(controlRateConfig_t *instance)
 
             .misc = {
                 .fpvCamAngleDegrees = 0,
-                .flipOverAfterPowerFactor = 65
             }
         );
     }

src/main/fc/controlrate_profile.h

@@ -64,7 +64,6 @@ typedef struct controlRateConfig_s {
 
     struct {
         uint8_t fpvCamAngleDegrees;             // Camera angle to treat as "forward" base axis in ACRO (Roll and Yaw sticks will command rotation considering this axis)
-        uint8_t flipOverAfterPowerFactor;
     } misc;
 
 } controlRateConfig_t;

src/main/fc/settings.yaml

@@ -722,6 +722,12 @@ groups:
         default_value: "14"
         min: 4
         max: 255
+      - name: flip_over_after_crash_power_factor
+        field: flipOverAfterPowerFactor
+        default_value: "65"
+        description: "flip over after crash power factor"
+        min: 0
+        max: 100
 
   - name: PG_FAILSAFE_CONFIG
     type: failsafeConfig_t
@@ -1159,12 +1165,6 @@ groups:
         field: misc.fpvCamAngleDegrees
         min: 0
         max: 50
-      - name: flip_over_after_crash_power_factor
-        field: misc.flipOverAfterPowerFactor
-        default_value: "65"
-        description: "flip over after crash power factor"
-        min: 0
-        max: 100
 
   - name: PG_SERIAL_CONFIG
     type: serialConfig_t

src/main/flight/mixer.c

@@ -100,7 +100,7 @@ PG_RESET_TEMPLATE(mixerConfig_t, mixerConfig,
 
 #define DEFAULT_MAX_THROTTLE    1850
 
-PG_REGISTER_WITH_RESET_TEMPLATE(motorConfig_t, motorConfig, PG_MOTOR_CONFIG, 6);
+PG_REGISTER_WITH_RESET_TEMPLATE(motorConfig_t, motorConfig, PG_MOTOR_CONFIG, 7);
 
 PG_RESET_TEMPLATE(motorConfig_t, motorConfig,
     .motorPwmProtocol = DEFAULT_PWM_PROTOCOL,
@@ -111,7 +111,8 @@ PG_RESET_TEMPLATE(motorConfig_t, motorConfig,
     .motorDecelTimeMs = 0,
     .throttleIdle = 15.0f,
     .throttleScale = 1.0f,
-    .motorPoleCount = 14            // Most brushless motors that we use are 14 poles
+    .motorPoleCount = 14,           // Most brushless motors that we use are 14 poles
+    .flipOverAfterPowerFactor = 65
 );
 
 PG_REGISTER_ARRAY(motorMixer_t, MAX_SUPPORTED_MOTORS, primaryMotorMixer, PG_MOTOR_MIXER, 0);
@@ -326,7 +327,7 @@ static uint16_t handleOutputScaling(
 static void applyFlipOverAfterCrashModeToMotors(void) {
 
     if (ARMING_FLAG(ARMED)) {
-        const float flipPowerFactor = ((float)currentControlRateProfile->misc.flipOverAfterPowerFactor/100.0f);
+        const float flipPowerFactor = ((float)motorConfig()->flipOverAfterPowerFactor)/100.0f;
         const float stickDeflectionPitchAbs = ABS(((float) rcCommand[PITCH]) / 500.0f);
         const float stickDeflectionRollAbs = ABS(((float) rcCommand[ROLL]) / 500.0f);
         const float stickDeflectionYawAbs = ABS(((float) rcCommand[YAW]) / 500.0f);

src/main/flight/mixer.h

@@ -92,6 +92,7 @@ typedef struct motorConfig_s {
     float throttleIdle;                     // Throttle IDLE value based on min_command, max_throttle, in percent
     float throttleScale;                    // Scaling factor for throttle.
     uint8_t motorPoleCount;                 // Magnetic poles in the motors for calculating actual RPM from eRPM provided by ESC telemetry
+    uint8_t flipOverAfterPowerFactor;       // Power factor from 0 to 100% of flip over after crash
 } motorConfig_t;
 
 PG_DECLARE(motorConfig_t, motorConfig);