|
|
|
@ -78,6 +78,24 @@ const AP_Param::GroupInfo AC_WPNav::var_info[] PROGMEM = {
@@ -78,6 +78,24 @@ const AP_Param::GroupInfo AC_WPNav::var_info[] PROGMEM = {
|
|
|
|
|
// @Increment: 1
|
|
|
|
|
// @User: Advanced
|
|
|
|
|
AP_GROUPINFO("LOIT_JERK", 7, AC_WPNav, _loiter_jerk_max_cmsss, WPNAV_LOITER_JERK_MAX_DEFAULT), |
|
|
|
|
|
|
|
|
|
// @Param: LOIT_MAXA
|
|
|
|
|
// @DisplayName: Loiter maximum acceleration
|
|
|
|
|
// @Description: Loiter maximum acceleration in cm/s/s
|
|
|
|
|
// @Units: cm/s/s
|
|
|
|
|
// @Range: 100 981
|
|
|
|
|
// @Increment: 1
|
|
|
|
|
// @User: Advanced
|
|
|
|
|
AP_GROUPINFO("LOIT_MAXA", 8, AC_WPNav, _loiter_accel_cmss, WPNAV_LOITER_ACCEL), |
|
|
|
|
|
|
|
|
|
// @Param: LOIT_MINA
|
|
|
|
|
// @DisplayName: Loiter minimum acceleration
|
|
|
|
|
// @Description: Loiter minimum acceleration in cm/s/s
|
|
|
|
|
// @Units: cm/s/s
|
|
|
|
|
// @Range: 100 981
|
|
|
|
|
// @Increment: 1
|
|
|
|
|
// @User: Advanced
|
|
|
|
|
AP_GROUPINFO("LOIT_MINA", 9, AC_WPNav, _loiter_accel_min_cmss, WPNAV_LOITER_ACCEL_MIN), |
|
|
|
|
|
|
|
|
|
AP_GROUPEND |
|
|
|
|
}; |
|
|
|
@ -94,7 +112,6 @@ AC_WPNav::AC_WPNav(const AP_InertialNav& inav, const AP_AHRS& ahrs, AC_PosContro
@@ -94,7 +112,6 @@ AC_WPNav::AC_WPNav(const AP_InertialNav& inav, const AP_AHRS& ahrs, AC_PosContro
|
|
|
|
|
_loiter_step(0), |
|
|
|
|
_pilot_accel_fwd_cms(0), |
|
|
|
|
_pilot_accel_rgt_cms(0), |
|
|
|
|
_loiter_accel_cms(WPNAV_LOITER_ACCEL), |
|
|
|
|
_wp_last_update(0), |
|
|
|
|
_wp_step(0), |
|
|
|
|
_track_length(0.0f), |
|
|
|
@ -124,8 +141,7 @@ void AC_WPNav::init_loiter_target(const Vector3f& position, bool reset_I)
@@ -124,8 +141,7 @@ void AC_WPNav::init_loiter_target(const Vector3f& position, bool reset_I)
|
|
|
|
|
|
|
|
|
|
// initialise pos controller speed and acceleration
|
|
|
|
|
_pos_control.set_speed_xy(_loiter_speed_cms); |
|
|
|
|
_loiter_accel_cms = _loiter_speed_cms/2.0f; |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cms); |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cmss); |
|
|
|
|
|
|
|
|
|
// set target position
|
|
|
|
|
_pos_control.set_xy_target(position.x, position.y); |
|
|
|
@ -153,8 +169,7 @@ void AC_WPNav::init_loiter_target()
@@ -153,8 +169,7 @@ void AC_WPNav::init_loiter_target()
|
|
|
|
|
|
|
|
|
|
// initialise pos controller speed and acceleration
|
|
|
|
|
_pos_control.set_speed_xy(_loiter_speed_cms); |
|
|
|
|
_loiter_accel_cms = _loiter_speed_cms/2.0f; |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cms); |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cmss); |
|
|
|
|
|
|
|
|
|
// set target position
|
|
|
|
|
_pos_control.set_xy_target(curr_pos.x, curr_pos.y); |
|
|
|
@ -163,8 +178,8 @@ void AC_WPNav::init_loiter_target()
@@ -163,8 +178,8 @@ void AC_WPNav::init_loiter_target()
|
|
|
|
|
_pos_control.set_desired_velocity_xy(curr_vel.x, curr_vel.y); |
|
|
|
|
|
|
|
|
|
// initialise desired accel and add fake wind
|
|
|
|
|
_loiter_desired_accel.x = (_loiter_accel_cms)*curr_vel.x/_loiter_speed_cms; |
|
|
|
|
_loiter_desired_accel.y = (_loiter_accel_cms)*curr_vel.y/_loiter_speed_cms; |
|
|
|
|
_loiter_desired_accel.x = (_loiter_accel_cmss)*curr_vel.x/_loiter_speed_cms; |
|
|
|
|
_loiter_desired_accel.y = (_loiter_accel_cmss)*curr_vel.y/_loiter_speed_cms; |
|
|
|
|
|
|
|
|
|
// initialise pilot input
|
|
|
|
|
_pilot_accel_fwd_cms = 0; |
|
|
|
@ -193,8 +208,7 @@ void AC_WPNav::set_loiter_velocity(float velocity_cms)
@@ -193,8 +208,7 @@ void AC_WPNav::set_loiter_velocity(float velocity_cms)
|
|
|
|
|
_pos_control.set_speed_xy(_loiter_speed_cms); |
|
|
|
|
|
|
|
|
|
// initialise pos controller acceleration
|
|
|
|
|
_loiter_accel_cms = _loiter_speed_cms/2.0f; |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cms); |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cmss); |
|
|
|
|
} |
|
|
|
|
} |
|
|
|
|
|
|
|
|
@ -202,8 +216,8 @@ void AC_WPNav::set_loiter_velocity(float velocity_cms)
@@ -202,8 +216,8 @@ void AC_WPNav::set_loiter_velocity(float velocity_cms)
|
|
|
|
|
void AC_WPNav::set_pilot_desired_acceleration(float control_roll, float control_pitch) |
|
|
|
|
{ |
|
|
|
|
// convert pilot input to desired acceleration in cm/s/s
|
|
|
|
|
_pilot_accel_fwd_cms = -control_pitch * _loiter_accel_cms / 4500.0f; |
|
|
|
|
_pilot_accel_rgt_cms = control_roll * _loiter_accel_cms / 4500.0f; |
|
|
|
|
_pilot_accel_fwd_cms = -control_pitch * _loiter_accel_cmss / 4500.0f; |
|
|
|
|
_pilot_accel_rgt_cms = control_roll * _loiter_accel_cmss / 4500.0f; |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
/// get_loiter_stopping_point_xy - returns vector to stopping point based on a horizontal position and velocity
|
|
|
|
@ -224,8 +238,10 @@ void AC_WPNav::calc_loiter_desired_velocity(float nav_dt, float ekfGndSpdLimit)
@@ -224,8 +238,10 @@ void AC_WPNav::calc_loiter_desired_velocity(float nav_dt, float ekfGndSpdLimit)
|
|
|
|
|
// check loiter speed and avoid divide by zero
|
|
|
|
|
if( _loiter_speed_cms < WPNAV_LOITER_SPEED_MIN) { |
|
|
|
|
_loiter_speed_cms = WPNAV_LOITER_SPEED_MIN; |
|
|
|
|
_loiter_accel_cms = _loiter_speed_cms/2.0f; |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
_pos_control.set_speed_xy(_loiter_speed_cms); |
|
|
|
|
_pos_control.set_accel_xy(_loiter_accel_cmss); |
|
|
|
|
|
|
|
|
|
// rotate pilot input to lat/lon frame
|
|
|
|
|
Vector2f desired_accel; |
|
|
|
@ -238,10 +254,12 @@ void AC_WPNav::calc_loiter_desired_velocity(float nav_dt, float ekfGndSpdLimit)
@@ -238,10 +254,12 @@ void AC_WPNav::calc_loiter_desired_velocity(float nav_dt, float ekfGndSpdLimit)
|
|
|
|
|
// constrain and scale the desired acceleration
|
|
|
|
|
float des_accel_change_total = pythagorous2(des_accel_diff.x, des_accel_diff.y); |
|
|
|
|
float accel_change_max = _loiter_jerk_max_cmsss * nav_dt; |
|
|
|
|
if (des_accel_change_total > accel_change_max && des_accel_change_total > 0.0f) { |
|
|
|
|
|
|
|
|
|
if (_loiter_jerk_max_cmsss > 0.0f && des_accel_change_total > accel_change_max && des_accel_change_total > 0.0f) { |
|
|
|
|
des_accel_diff.x = accel_change_max * des_accel_diff.x/des_accel_change_total; |
|
|
|
|
des_accel_diff.y = accel_change_max * des_accel_diff.y/des_accel_change_total; |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
// adjust the desired acceleration
|
|
|
|
|
_loiter_desired_accel += des_accel_diff; |
|
|
|
|
|
|
|
|
@ -252,22 +270,21 @@ void AC_WPNav::calc_loiter_desired_velocity(float nav_dt, float ekfGndSpdLimit)
@@ -252,22 +270,21 @@ void AC_WPNav::calc_loiter_desired_velocity(float nav_dt, float ekfGndSpdLimit)
|
|
|
|
|
desired_vel.x += _loiter_desired_accel.x * nav_dt; |
|
|
|
|
desired_vel.y += _loiter_desired_accel.y * nav_dt; |
|
|
|
|
|
|
|
|
|
// reduce velocity with fake wind resistance
|
|
|
|
|
if (_pilot_accel_fwd_cms != 0.0f || _pilot_accel_rgt_cms != 0.0f) { |
|
|
|
|
desired_vel.x -= (_loiter_accel_cms)*nav_dt*desired_vel.x/_loiter_speed_cms; |
|
|
|
|
desired_vel.y -= (_loiter_accel_cms)*nav_dt*desired_vel.y/_loiter_speed_cms; |
|
|
|
|
desired_vel.x -= (_loiter_accel_cmss)*nav_dt*desired_vel.x/_loiter_speed_cms; |
|
|
|
|
desired_vel.y -= (_loiter_accel_cmss)*nav_dt*desired_vel.y/_loiter_speed_cms; |
|
|
|
|
} else { |
|
|
|
|
desired_vel.x -= (_loiter_accel_cms-WPNAV_LOITER_ACCEL_MIN)*nav_dt*desired_vel.x/_loiter_speed_cms; |
|
|
|
|
desired_vel.x -= (_loiter_accel_cmss-_loiter_accel_min_cmss)*nav_dt*desired_vel.x/_loiter_speed_cms; |
|
|
|
|
if(desired_vel.x > 0 ) { |
|
|
|
|
desired_vel.x = max(desired_vel.x - WPNAV_LOITER_ACCEL_MIN*nav_dt, 0); |
|
|
|
|
desired_vel.x = max(desired_vel.x - _loiter_accel_min_cmss*nav_dt, 0); |
|
|
|
|
}else if(desired_vel.x < 0) { |
|
|
|
|
desired_vel.x = min(desired_vel.x + WPNAV_LOITER_ACCEL_MIN*nav_dt, 0); |
|
|
|
|
desired_vel.x = min(desired_vel.x + _loiter_accel_min_cmss*nav_dt, 0); |
|
|
|
|
} |
|
|
|
|
desired_vel.y -= (_loiter_accel_cms-WPNAV_LOITER_ACCEL_MIN)*nav_dt*desired_vel.y/_loiter_speed_cms; |
|
|
|
|
desired_vel.y -= (_loiter_accel_cmss-_loiter_accel_min_cmss)*nav_dt*desired_vel.y/_loiter_speed_cms; |
|
|
|
|
if(desired_vel.y > 0 ) { |
|
|
|
|
desired_vel.y = max(desired_vel.y - WPNAV_LOITER_ACCEL_MIN*nav_dt, 0); |
|
|
|
|
desired_vel.y = max(desired_vel.y - _loiter_accel_min_cmss*nav_dt, 0); |
|
|
|
|
}else if(desired_vel.y < 0) { |
|
|
|
|
desired_vel.y = min(desired_vel.y + WPNAV_LOITER_ACCEL_MIN*nav_dt, 0); |
|
|
|
|
desired_vel.y = min(desired_vel.y + _loiter_accel_min_cmss*nav_dt, 0); |
|
|
|
|
} |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|