Ejemplo n.º 1
0
/*
float vector_magnitude(float quadrature_component, float direct_component)
{
	float magnitude;
	magnitude=sqrtf( (quadrature_component*quadrature_component+direct_component*direct_component) );
	return magnitude;
}


float vector_angle(float quadrature_component, float direct_component)
{
	float angle;
	//angle=180.0f/PI*atanf(quadrature_component/direct_component);
	angle=57.295779513082320f*atanf(quadrature_component/direct_component);

	

	if (angle>=360.0f)
		angle=angle-360.0f;
	else if (angle<0.0f)
		angle=angle+360.0f;

	if ( (quadrature_component<=0.0f) && (direct_component<0.0f) )
		angle=angle+180.0f;

	else if ( (quadrature_component>0.0f)&&(direct_component<0.0f))
		angle=angle-180.0f;

	return angle;
}
*/
float fast_vector_angle(float y, float x)
{
  float angle;
/*
  if      (x>=0.0f && y>=0.0f &&  x>= y) { angle =        fast_atan( y/ x); }  //1st quadrant
  else if (x>=0.0f && y>=0.0f &&  y> x)  { angle =  90.0f-fast_atan( x/ y); }  //2nd quadrant
  else if (x< 0.0f && y>=0.0f &&  y>=-x) { angle =  90.0f+fast_atan(-x/ y); }  //3rd quadrant
  else if (x< 0.0f && y>=0.0f && -x> y)  { angle = 180.0f-fast_atan( y/-x); }  //4th quadrant
  else if (x< 0.0f && y< 0.0f && -x>=-y) { angle = 180.0f+fast_atan(-y/-x); }  //5th quadrant
  else if (x< 0.0f && y< 0.0f && -y>-x)  { angle = 270.0f-fast_atan(-x/-y); }  //6th quadrant
  else if (x>=0.0f && y< 0.0f && -y>= x) { angle = 270.0f+fast_atan( x/-y); }  //7th quadrant 
  else if (x>=0.0f && y< 0.0f &&  x>-y)  { angle = 360.0f-fast_atan(-y/ x); }  //8th quadrant 
  else                                   { angle =   0.0f                 ; }  //lost quadrant
*/
  if      (x>=0.0f && y>=0.0f &&  x>= y) { angle =        fast_atan( y/ x); }  //1st quadrant
  else if (x>=0.0f && y>=0.0f &&  y> x)  { angle =  90.0f-fast_atan( x/ y); }  //2nd quadrant
  else if (x< 0.0f && y>=0.0f &&  y>=-x) { angle =  90.0f+fast_atan(-x/ y); }  //3rd quadrant
  else if (x< 0.0f && y>=0.0f && -x> y)  { angle = 180.0f-fast_atan( y/-x); }  //4th quadrant
  else if (x< 0.0f && y< 0.0f && -x>=-y) { angle = 180.0f+fast_atan(-y/-x); }  //5th quadrant
  else if (x< 0.0f && y< 0.0f && -y>-x)  { angle = 270.0f-fast_atan(-x/-y); }  //6th quadrant
  else if (x>=0.0f && y< 0.0f && -y>= x) { angle = 270.0f+fast_atan( x/-y); }  //7th quadrant 
  else if (x>=0.0f && y< 0.0f &&  x>-y)  { angle = 360.0f-fast_atan(-y/ x); }  //8th quadrant 
  else                                   { angle =   0.0f                 ; }

  return angle;
}
Ejemplo n.º 2
0
/// accel_to_lean_angles - horizontal desired acceleration to lean angles
///    converts desired accelerations provided in lat/lon frame to roll/pitch angles
void AC_PosControl::accel_to_lean_angles()
{
    float accel_right, accel_forward;
    float lean_angle_max = _attitude_control.lean_angle_max();

    // To-Do: add 1hz filter to accel_lat, accel_lon

    // rotate accelerations into body forward-right frame
    accel_forward = _accel_target.x*_ahrs.cos_yaw() + _accel_target.y*_ahrs.sin_yaw();
    accel_right = -_accel_target.x*_ahrs.sin_yaw() + _accel_target.y*_ahrs.cos_yaw();

    // update angle targets that will be passed to stabilize controller
    _roll_target = constrain_float(fast_atan(accel_right*_ahrs.cos_pitch()/(GRAVITY_MSS * 100))*(18000/M_PI), -lean_angle_max, lean_angle_max);
    _pitch_target = constrain_float(fast_atan(-accel_forward/(GRAVITY_MSS * 100))*(18000/M_PI),-lean_angle_max, lean_angle_max);
}
Ejemplo n.º 3
0
/// get_loiter_acceleration_to_lean_angles - loiter acceleration controller
///    converts desired accelerations provided in lat/lon frame to roll/pitch angles
void AC_WPNav::get_loiter_acceleration_to_lean_angles(float accel_lat, float accel_lon)
{
    float z_accel_meas = -GRAVITY_MSS * 100;    // gravity in cm/s/s
    float accel_forward;
    float accel_right;

    // To-Do: add 1hz filter to accel_lat, accel_lon

    // rotate accelerations into body forward-right frame
    accel_forward = accel_lat*_cos_yaw + accel_lon*_sin_yaw;
    accel_right = -accel_lat*_sin_yaw + accel_lon*_cos_yaw;

    // update angle targets that will be passed to stabilize controller
    _desired_roll = constrain_float(fast_atan(accel_right*_cos_pitch/(-z_accel_meas))*(18000/M_PI), -MAX_LEAN_ANGLE, MAX_LEAN_ANGLE);
    _desired_pitch = constrain_float(fast_atan(-accel_forward/(-z_accel_meas))*(18000/M_PI), -MAX_LEAN_ANGLE, MAX_LEAN_ANGLE);
}
Ejemplo n.º 4
0
/// accel_to_lean_angles - horizontal desired acceleration to lean angles
///    converts desired accelerations provided in lat/lon frame to roll/pitch angles
void AC_PosControl::accel_to_lean_angles(float dt, float ekfNavVelGainScaler)
{
    float accel_right, accel_forward;
    float lean_angle_max = _attitude_control.lean_angle_max();

    // reset accel to current desired acceleration
    if (_flags.reset_accel_to_lean_xy) {
        _accel_target_jerk_limited.x = _accel_target.x;
        _accel_target_jerk_limited.y = _accel_target.y;
        _accel_target_filtered.x = _accel_target.x;
        _accel_target_filtered.y = _accel_target.y;
        _flags.reset_accel_to_lean_xy = false;
    }

    // apply jerk limit of 17 m/s^3 - equates to a worst case of about 100 deg/sec/sec
    float max_delta_accel = dt * POSCONTROL_JERK_LIMIT_CMSSS;

    Vector2f accel_in(_accel_target.x, _accel_target.y);
    Vector2f accel_change = accel_in-_accel_target_jerk_limited;
    float accel_change_length = accel_change.length();

    if(accel_change_length > max_delta_accel) {
        accel_change *= max_delta_accel/accel_change_length;
    }
    _accel_target_jerk_limited += accel_change;

    // 5Hz lowpass filter on NE accel
    float freq_cut = POSCONTROL_ACCEL_FILTER_HZ * ekfNavVelGainScaler;
    float alpha = constrain_float(dt/(dt + 1.0f/(2.0f*(float)M_PI*freq_cut)),0.0f,1.0f);
    _accel_target_filtered.x += alpha * (_accel_target_jerk_limited.x - _accel_target_filtered.x);
    _accel_target_filtered.y  += alpha * (_accel_target_jerk_limited.y - _accel_target_filtered.y);

    // rotate accelerations into body forward-right frame
    accel_forward = _accel_target_filtered.x*_ahrs.cos_yaw() + _accel_target_filtered.y*_ahrs.sin_yaw();
    accel_right = -_accel_target_filtered.x*_ahrs.sin_yaw() + _accel_target_filtered.y*_ahrs.cos_yaw();

    // update angle targets that will be passed to stabilize controller
    _pitch_target = constrain_float(fast_atan(-accel_forward/(GRAVITY_MSS * 100))*(18000/M_PI),-lean_angle_max, lean_angle_max);
    float cos_pitch_target = cosf(_pitch_target*(float)M_PI/18000);
    _roll_target = constrain_float(fast_atan(accel_right*cos_pitch_target/(GRAVITY_MSS * 100))*(18000/M_PI), -lean_angle_max, lean_angle_max);
}