guidance_indi_hybrid_quadplane.h File Reference

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Macros
#define	GUIDANCE_INDI_MIN_PITCH   -20
#define	GUIDANCE_INDI_MAX_PITCH   20

Functions
void	guidance_indi_quadplane_init (void)
	Call upon entering indi guidance.
void	guidance_indi_quadplane_propagate_filters (void)
	Low pass the accelerometer measurements to remove noise from vibrations.

Macro Definition Documentation

GUIDANCE_INDI_MAX_PITCH

#define GUIDANCE_INDI_MAX_PITCH   20

Definition at line 32 of file guidance_indi_hybrid_quadplane.h.

GUIDANCE_INDI_MIN_PITCH

#define GUIDANCE_INDI_MIN_PITCH   -20

Definition at line 31 of file guidance_indi_hybrid_quadplane.h.

Function Documentation

guidance_indi_quadplane_init()

void guidance_indi_quadplane_init ( void  )

extern

Call upon entering indi guidance.

Definition at line 61 of file guidance_indi_hybrid_quadplane.c.

References accel_bodyz_filt, foo, GUIDANCE_INDI_BODYZ_FILTER_CUTOFF, and init_butterworth_2_low_pass().

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guidance_indi_quadplane_propagate_filters()

void guidance_indi_quadplane_propagate_filters ( void  )

extern

Low pass the accelerometer measurements to remove noise from vibrations.

The roll and pitch also need to be filtered to synchronize them with the acceleration Called as a periodic function with PERIODIC_FREQ

Definition at line 73 of file guidance_indi_hybrid_quadplane.c.

References accel_bodyz_filt, ACCEL_FLOAT_OF_BFP, foo, stateGetAccelBody_i(), and update_butterworth_2_low_pass().

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