void stabilization_attitude_run(bool_t enable_integrator)
{

  /*
   * Update reference
   */
  stabilization_attitude_ref_update();

  /*
   * Compute errors for feedback
   */

  /* attitude error                          */
  struct Int32Quat att_err;
  struct Int32Quat *att_quat = stateGetNedToBodyQuat_i();
  INT32_QUAT_INV_COMP(att_err, *att_quat, stab_att_ref_quat);
  /* wrap it in the shortest direction       */
  int32_quat_wrap_shortest(&att_err);
  int32_quat_normalize(&att_err);

  /*  rate error                */
  const struct Int32Rates rate_ref_scaled = {
    OFFSET_AND_ROUND(stab_att_ref_rate.p, (REF_RATE_FRAC - INT32_RATE_FRAC)),
    OFFSET_AND_ROUND(stab_att_ref_rate.q, (REF_RATE_FRAC - INT32_RATE_FRAC)),
    OFFSET_AND_ROUND(stab_att_ref_rate.r, (REF_RATE_FRAC - INT32_RATE_FRAC))
  };
  struct Int32Rates rate_err;
  struct Int32Rates *body_rate = stateGetBodyRates_i();
  RATES_DIFF(rate_err, rate_ref_scaled, (*body_rate));

#define INTEGRATOR_BOUND 100000
  /* integrated error */
  if (enable_integrator) {
    stabilization_att_sum_err_quat.qx += att_err.qx / IERROR_SCALE;
    stabilization_att_sum_err_quat.qy += att_err.qy / IERROR_SCALE;
    stabilization_att_sum_err_quat.qz += att_err.qz / IERROR_SCALE;
    Bound(stabilization_att_sum_err_quat.qx, -INTEGRATOR_BOUND, INTEGRATOR_BOUND);
    Bound(stabilization_att_sum_err_quat.qy, -INTEGRATOR_BOUND, INTEGRATOR_BOUND);
    Bound(stabilization_att_sum_err_quat.qz, -INTEGRATOR_BOUND, INTEGRATOR_BOUND);
  } else {
    /* reset accumulator */
    int32_quat_identity(&stabilization_att_sum_err_quat);
  }

  /* compute the feed forward command */
  attitude_run_ff(stabilization_att_ff_cmd, &stabilization_gains, &stab_att_ref_accel);

  /* compute the feed back command */
  attitude_run_fb(stabilization_att_fb_cmd, &stabilization_gains, &att_err, &rate_err, &stabilization_att_sum_err_quat);

  /* sum feedforward and feedback */
  stabilization_cmd[COMMAND_ROLL] = stabilization_att_fb_cmd[COMMAND_ROLL] + stabilization_att_ff_cmd[COMMAND_ROLL];
  stabilization_cmd[COMMAND_PITCH] = stabilization_att_fb_cmd[COMMAND_PITCH] + stabilization_att_ff_cmd[COMMAND_PITCH];
  stabilization_cmd[COMMAND_YAW] = stabilization_att_fb_cmd[COMMAND_YAW] + stabilization_att_ff_cmd[COMMAND_YAW];

  /* bound the result */
  BoundAbs(stabilization_cmd[COMMAND_ROLL], MAX_PPRZ);
  BoundAbs(stabilization_cmd[COMMAND_PITCH], MAX_PPRZ);
  BoundAbs(stabilization_cmd[COMMAND_YAW], MAX_PPRZ);
}
void stabilization_attitude_run(bool_t enable_integrator) {

  /*
   * Update reference
   */
  stabilization_attitude_ref_update();

  /*
   * Compute errors for feedback
   */

  /* attitude error                          */
  struct Int32Quat att_err;
  struct Int32Quat* att_quat = stateGetNedToBodyQuat_i();
  INT32_QUAT_INV_COMP(att_err, *att_quat, stab_att_ref_quat);
  /* wrap it in the shortest direction       */
  INT32_QUAT_WRAP_SHORTEST(att_err);
  INT32_QUAT_NORMALIZE(att_err);

  /*  rate error                */
  struct Int32Rates rate_err;
  struct Int32Rates* body_rate = stateGetBodyRates_i();
  RATES_DIFF(rate_err, stab_att_ref_rate, *body_rate);

  /* integrated error */
  if (enable_integrator) {
    struct Int32Quat new_sum_err, scaled_att_err;
    /* update accumulator */
    scaled_att_err.qi = att_err.qi;
    scaled_att_err.qx = att_err.qx / IERROR_SCALE;
    scaled_att_err.qy = att_err.qy / IERROR_SCALE;
    scaled_att_err.qz = att_err.qz / IERROR_SCALE;
    INT32_QUAT_COMP(new_sum_err, stabilization_att_sum_err_quat, scaled_att_err);
    INT32_QUAT_NORMALIZE(new_sum_err);
    QUAT_COPY(stabilization_att_sum_err_quat, new_sum_err);
    INT32_EULERS_OF_QUAT(stabilization_att_sum_err, stabilization_att_sum_err_quat);
  } else {
    /* reset accumulator */
    INT32_QUAT_ZERO( stabilization_att_sum_err_quat );
    INT_EULERS_ZERO( stabilization_att_sum_err );
  }

  /* compute the feed forward command */
  attitude_run_ff(stabilization_att_ff_cmd, &stabilization_gains, &stab_att_ref_accel);

  /* compute the feed back command */
  attitude_run_fb(stabilization_att_fb_cmd, &stabilization_gains, &att_err, &rate_err, &stabilization_att_sum_err_quat);

  /* sum feedforward and feedback */
  stabilization_cmd[COMMAND_ROLL] = stabilization_att_fb_cmd[COMMAND_ROLL] + stabilization_att_ff_cmd[COMMAND_ROLL];
  stabilization_cmd[COMMAND_PITCH] = stabilization_att_fb_cmd[COMMAND_PITCH] + stabilization_att_ff_cmd[COMMAND_PITCH];
  stabilization_cmd[COMMAND_YAW] = stabilization_att_fb_cmd[COMMAND_YAW] + stabilization_att_ff_cmd[COMMAND_YAW];

  /* bound the result */
  BoundAbs(stabilization_cmd[COMMAND_ROLL], MAX_PPRZ);
  BoundAbs(stabilization_cmd[COMMAND_PITCH], MAX_PPRZ);
  BoundAbs(stabilization_cmd[COMMAND_YAW], MAX_PPRZ);
}
void stabilization_attitude_run(bool_t enable_integrator) {

  /*
   * Update reference
   */
  stabilization_attitude_ref_update();

  /*
   * Compute errors for feedback
   */

  /* attitude error                          */
  struct Int32Quat att_err;
  INT32_QUAT_INV_COMP(att_err, ahrs.ltp_to_body_quat, stab_att_ref_quat);
  /* wrap it in the shortest direction       */
  INT32_QUAT_WRAP_SHORTEST(att_err);
  INT32_QUAT_NORMALIZE(att_err);

  /*  rate error                */
  struct Int32Rates rate_err;
  RATES_DIFF(rate_err, ahrs.body_rate, stab_att_ref_rate);

  /* integrated error */
  if (enable_integrator) {
    struct Int32Quat new_sum_err, scaled_att_err;
    /* update accumulator */
    scaled_att_err.qi = att_err.qi;
    scaled_att_err.qx = att_err.qx / IERROR_SCALE;
    scaled_att_err.qy = att_err.qy / IERROR_SCALE;
    scaled_att_err.qz = att_err.qz / IERROR_SCALE;
    INT32_QUAT_COMP_INV(new_sum_err, stabilization_att_sum_err_quat, scaled_att_err);
    INT32_QUAT_NORMALIZE(new_sum_err);
    QUAT_COPY(stabilization_att_sum_err_quat, new_sum_err);
    INT32_EULERS_OF_QUAT(stabilization_att_sum_err, stabilization_att_sum_err_quat);
  } else {
    /* reset accumulator */
    INT32_QUAT_ZERO( stabilization_att_sum_err_quat );
    INT_EULERS_ZERO( stabilization_att_sum_err );
  }

  attitude_run_ff(stabilization_att_ff_cmd, current_stabilization_gains, &stab_att_ref_accel);

  attitude_run_fb(stabilization_att_fb_cmd, current_stabilization_gains, &att_err, &rate_err, &stabilization_att_sum_err_quat);

  for (int i = COMMAND_ROLL; i <= COMMAND_YAW; i++) {
    stabilization_cmd[i] = stabilization_att_fb_cmd[i]+stabilization_att_ff_cmd[i];
     Bound(stabilization_cmd[i], -200, 200);
  }
}