ahrs_int_cmpl_quat.h

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/*
 * Copyright (C) 2008-2013 The Paparazzi Team
 *
 * This file is part of paparazzi.
 *
 * paparazzi is free software; you can redistribute it and/or modify
 * it under the terms of the GNU General Public License as published by
 * the Free Software Foundation; either version 2, or (at your option)
 * any later version.
 *
 * paparazzi is distributed in the hope that it will be useful,
 * but WITHOUT ANY WARRANTY; without even the implied warranty of
 * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
 * GNU General Public License for more details.
 *
 * You should have received a copy of the GNU General Public License
 * along with paparazzi; see the file COPYING.  If not, write to
 * the Free Software Foundation, 59 Temple Place - Suite 330,
 * Boston, MA 02111-1307, USA.
 */
 
#ifndef AHRS_INT_CMPL_QUAT_H
#define AHRS_INT_CMPL_QUAT_H
 
#include "modules/ahrs/ahrs.h"
#include "modules/gps/gps.h"
#include "std.h"
#include "math/pprz_algebra_int.h"
#include "math/pprz_orientation_conversion.h"
 
enum AhrsICQStatus {
  AHRS_ICQ_UNINIT,
  AHRS_ICQ_RUNNING
};
 
struct AhrsIntCmplQuat {
  struct Int32Rates  gyro_bias;
  struct Int32Rates  body_rate;
  struct Int32Rates  rate_correction;
  struct Int64Quat   high_rez_quat;
  struct Int64Rates  high_rez_bias;
  struct Int32Quat   ltp_to_body_quat;
  struct Int32Vect3  mag_h;
 
  int32_t ltp_vel_norm;
  bool ltp_vel_norm_valid;
  bool heading_aligned;
  float weight;
  float accel_inv_kp;
  float accel_inv_ki;
  float mag_kp;
  float mag_ki;
 
  /* parameters/options that can be changed */
  bool correct_gravity;
 
  uint8_t gravity_heuristic_factor;
 
  float accel_omega;
 
  float accel_zeta;
 
  float mag_omega;
 
  float mag_zeta;
 
  /* internal counters for the gains */
  uint16_t accel_cnt; 
  uint16_t mag_cnt;   
 
  enum AhrsICQStatus status; 
  bool is_aligned;
};
 
extern struct AhrsIntCmplQuat ahrs_icq;
 
extern void ahrs_icq_init(void);
extern bool ahrs_icq_align(struct Int32Rates *lp_gyro, struct Int32Vect3 *lp_accel,
                             struct Int32Vect3 *lp_mag);
extern void ahrs_icq_propagate(struct Int32Rates *gyro, float dt);
extern void ahrs_icq_update_accel(struct Int32Vect3 *accel, float dt);
extern void ahrs_icq_update_mag(struct Int32Vect3 *mag, float dt);
extern void ahrs_icq_update_gps(struct GpsState *gps_s);
 
void ahrs_icq_update_heading(int32_t heading);
 
void ahrs_icq_realign_heading(int32_t heading);
 
 
extern void ahrs_icq_set_accel_gains(void);
 
static inline void ahrs_int_cmpl_quat_SetAccelOmega(float omega)
{
  ahrs_icq.accel_omega = omega;
  ahrs_icq_set_accel_gains();
}
 
static inline void ahrs_int_cmpl_quat_SetAccelZeta(float zeta)
{
  ahrs_icq.accel_zeta = zeta;
  ahrs_icq_set_accel_gains();
}
 
extern void ahrs_icq_set_mag_gains(void);
 
static inline void ahrs_int_cmpl_quat_SetMagOmega(float omega)
{
  ahrs_icq.mag_omega = omega;
  ahrs_icq_set_mag_gains();
}
 
static inline void ahrs_int_cmpl_quat_SetMagZeta(float zeta)
{
  ahrs_icq.mag_zeta = zeta;
  ahrs_icq_set_mag_gains();
}
 
 
#endif /* AHRS_INT_CMPL_QUAT_H */