/* fake generated airframe file */

#ifndef AIRFRAME_H
#define AIRFRAME_H

#define PERIODIC_FREQUENCY 512

#if defined STABILIZATION_ATTITUDE_TYPE_FLOAT

#define STABILIZATION_ATTITUDE_REF_OMEGA_P {RadOfDeg(400)}
#define STABILIZATION_ATTITUDE_REF_ZETA_P {0.85}

#define STABILIZATION_ATTITUDE_REF_OMEGA_Q {RadOfDeg(400)}
#define STABILIZATION_ATTITUDE_REF_ZETA_Q {0.85}

#define STABILIZATION_ATTITUDE_REF_OMEGA_R {RadOfDeg(250)}
#define STABILIZATION_ATTITUDE_REF_ZETA_R {0.85}

#elif defined STABILIZATION_ATTITUDE_TYPE_INT

#define STABILIZATION_ATTITUDE_REF_OMEGA_P 6.981317
#define STABILIZATION_ATTITUDE_REF_ZETA_P 0.85

#define STABILIZATION_ATTITUDE_REF_OMEGA_Q 6.981317
#define STABILIZATION_ATTITUDE_REF_ZETA_Q 0.85

#define STABILIZATION_ATTITUDE_REF_OMEGA_R 4.363323125
#define STABILIZATION_ATTITUDE_REF_ZETA_R 0.85

#endif


#endif // AIRFRAME_H
