30 #ifndef GUIDANCE_INDI_H
31 #define GUIDANCE_INDI_H
void guidance_indi_enter(void)
Call upon entering indi guidance.
float guidance_indi_thrust_specific_force_gain
void guidance_indi_filter_accel(void)
low pass the accelerometer measurements with a second order filter to remove noise from vibrations ...
void guidance_indi_filter_thrust(void)
void stabilization_attitude_set_setpoint_rp_quat_f(struct FloatEulers *indi_rp_cmd, bool in_flight, int32_t heading)
Paparazzi floating point algebra.
void guidance_indi_run(bool in_flight, int32_t heading)
void guidance_indi_filter_attitude(void)
Filter the attitude, such that it corresponds to the filtered measured acceleration.
void guidance_indi_calcG(struct FloatMat33 *Gmat)
Paparazzi fixed point algebra.