mirror of https://github.com/ArduPilot/ardupilot
Copter: remove unused Ch6 EKF tuning options
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@ -57,9 +57,9 @@ enum tuning_func {
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TUNING_CIRCLE_RATE = 39, // circle turn rate in degrees (hard coded to about 45 degrees in either direction)
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TUNING_ACRO_YAW_KP = 40, // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate
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TUNING_RANGEFINDER_GAIN = 41, // rangefinder gain
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TUNING_EKF_VERTICAL_POS = 42, // EKF's baro vs accel (higher rely on accels more, baro impact is reduced). Range should be 0.2 ~ 4.0? 2.0 is default
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TUNING_EKF_HORIZONTAL_POS = 43, // EKF's gps vs accel (higher rely on accels more, gps impact is reduced). Range should be 1.0 ~ 3.0? 1.5 is default
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TUNING_EKF_ACCEL_NOISE = 44, // EKF's accel noise (lower means trust accels more, gps & baro less). Range should be 0.02 ~ 0.5 0.5 is default (but very robust at that level)
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TUNING_EKF_VERTICAL_POS = 42, // unused
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TUNING_EKF_HORIZONTAL_POS = 43, // unused
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TUNING_EKF_ACCEL_NOISE = 44, // unused
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TUNING_RC_FEEL_RP = 45, // roll-pitch input smoothing
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TUNING_RATE_PITCH_KP = 46, // body frame pitch rate controller's P term
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TUNING_RATE_PITCH_KI = 47, // body frame pitch rate controller's I term
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@ -149,37 +149,6 @@ void Copter::tuning()
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break;
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#endif
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#if 0
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// disabled for now - we need accessor functions
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case TUNING_EKF_VERTICAL_POS:
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// Tune the EKF that is being used
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// EKF's baro vs accel (higher rely on accels more, baro impact is reduced)
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if (!ahrs.get_NavEKF2().enabled()) {
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ahrs.get_NavEKF()._gpsVertPosNoise = tuning_value;
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} else {
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ahrs.get_NavEKF2()._gpsVertPosNoise = tuning_value;
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}
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break;
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case TUNING_EKF_HORIZONTAL_POS:
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// EKF's gps vs accel (higher rely on accels more, gps impact is reduced)
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if (!ahrs.get_NavEKF2().enabled()) {
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ahrs.get_NavEKF()._gpsHorizPosNoise = tuning_value;
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} else {
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ahrs.get_NavEKF2()._gpsHorizPosNoise = tuning_value;
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}
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break;
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case TUNING_EKF_ACCEL_NOISE:
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// EKF's accel noise (lower means trust accels more, gps & baro less)
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if (!ahrs.get_NavEKF2().enabled()) {
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ahrs.get_NavEKF()._accNoise = tuning_value;
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} else {
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ahrs.get_NavEKF2()._accNoise = tuning_value;
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}
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break;
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#endif
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case TUNING_RC_FEEL_RP:
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attitude_control->set_input_tc(tuning_value);
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break;
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