|
|
|
@ -48,7 +48,7 @@ void Copter::ModeFollow::run()
@@ -48,7 +48,7 @@ void Copter::ModeFollow::run()
|
|
|
|
|
// position and velocity requests will be ignored while the vehicle is not in guided mode
|
|
|
|
|
|
|
|
|
|
// variables to be sent to velocity controller
|
|
|
|
|
Vector3f desired_velocity; |
|
|
|
|
Vector3f desired_velocity_neu_cms; |
|
|
|
|
bool use_yaw = false; |
|
|
|
|
float yaw_cd = 0.0f; |
|
|
|
|
|
|
|
|
@ -69,21 +69,21 @@ void Copter::ModeFollow::run()
@@ -69,21 +69,21 @@ void Copter::ModeFollow::run()
|
|
|
|
|
|
|
|
|
|
// calculate desired velocity vector in cm/s in NEU
|
|
|
|
|
const float kp = g2.follow.get_pos_p().kP(); |
|
|
|
|
desired_velocity.x = (vel_of_target.x * 100.0f) + (dist_vec_offs_neu.x * kp); |
|
|
|
|
desired_velocity.y = (vel_of_target.y * 100.0f) + (dist_vec_offs_neu.y * kp); |
|
|
|
|
desired_velocity.z = (-vel_of_target.z * 100.0f) + (dist_vec_offs_neu.z * kp); |
|
|
|
|
desired_velocity_neu_cms.x = (vel_of_target.x * 100.0f) + (dist_vec_offs_neu.x * kp); |
|
|
|
|
desired_velocity_neu_cms.y = (vel_of_target.y * 100.0f) + (dist_vec_offs_neu.y * kp); |
|
|
|
|
desired_velocity_neu_cms.z = (-vel_of_target.z * 100.0f) + (dist_vec_offs_neu.z * kp); |
|
|
|
|
|
|
|
|
|
// scale desired velocity to stay within horizontal speed limit
|
|
|
|
|
float desired_speed_xy = safe_sqrt(sq(desired_velocity.x) + sq(desired_velocity.y)); |
|
|
|
|
float desired_speed_xy = safe_sqrt(sq(desired_velocity_neu_cms.x) + sq(desired_velocity_neu_cms.y)); |
|
|
|
|
if (!is_zero(desired_speed_xy) && (desired_speed_xy > pos_control->get_speed_xy())) { |
|
|
|
|
const float scalar_xy = pos_control->get_speed_xy() / desired_speed_xy; |
|
|
|
|
desired_velocity.x *= scalar_xy; |
|
|
|
|
desired_velocity.y *= scalar_xy; |
|
|
|
|
desired_velocity_neu_cms.x *= scalar_xy; |
|
|
|
|
desired_velocity_neu_cms.y *= scalar_xy; |
|
|
|
|
desired_speed_xy = pos_control->get_speed_xy(); |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
// limit desired velocity to be between maximum climb and descent rates
|
|
|
|
|
desired_velocity.z = constrain_float(desired_velocity.z, -fabsf(pos_control->get_speed_down()), pos_control->get_speed_up()); |
|
|
|
|
desired_velocity_neu_cms.z = constrain_float(desired_velocity_neu_cms.z, -fabsf(pos_control->get_speed_down()), pos_control->get_speed_up()); |
|
|
|
|
|
|
|
|
|
// unit vector towards target position (i.e. vector to lead vehicle + offset)
|
|
|
|
|
Vector3f dir_to_target_neu = dist_vec_offs_neu; |
|
|
|
@ -93,31 +93,31 @@ void Copter::ModeFollow::run()
@@ -93,31 +93,31 @@ void Copter::ModeFollow::run()
|
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
// create horizontal desired velocity vector (required for slow down calculations)
|
|
|
|
|
Vector2f desired_velocity_xy(desired_velocity.x, desired_velocity.y); |
|
|
|
|
Vector2f desired_velocity_xy_cms(desired_velocity_neu_cms.x, desired_velocity_neu_cms.y); |
|
|
|
|
|
|
|
|
|
// create horizontal unit vector towards target (required for slow down calculations)
|
|
|
|
|
Vector2f dir_to_target_xy(desired_velocity_xy.x, desired_velocity_xy.y); |
|
|
|
|
Vector2f dir_to_target_xy(desired_velocity_xy_cms.x, desired_velocity_xy_cms.y); |
|
|
|
|
if (!dir_to_target_xy.is_zero()) { |
|
|
|
|
dir_to_target_xy.normalize(); |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
// slow down horizontally as we approach target (use 1/2 of maximum deceleration for gentle slow down)
|
|
|
|
|
const float dist_to_target_xy = Vector2f(dist_vec_offs_neu.x, dist_vec_offs_neu.y).length(); |
|
|
|
|
copter.avoid.limit_velocity(pos_control->get_pos_xy_p().kP().get(), pos_control->get_accel_xy() * 0.5f, desired_velocity_xy, dir_to_target_xy, dist_to_target_xy, copter.G_Dt); |
|
|
|
|
copter.avoid.limit_velocity(pos_control->get_pos_xy_p().kP().get(), pos_control->get_accel_xy() * 0.5f, desired_velocity_xy_cms, dir_to_target_xy, dist_to_target_xy, copter.G_Dt); |
|
|
|
|
|
|
|
|
|
// limit the horizontal velocity to prevent fence violations
|
|
|
|
|
copter.avoid.adjust_velocity(pos_control->get_pos_xy_p().kP().get(), pos_control->get_accel_xy(), desired_velocity_xy, G_Dt); |
|
|
|
|
copter.avoid.adjust_velocity(pos_control->get_pos_xy_p().kP().get(), pos_control->get_accel_xy(), desired_velocity_xy_cms, G_Dt); |
|
|
|
|
|
|
|
|
|
// copy horizontal velocity limits back to 3d vector
|
|
|
|
|
desired_velocity.x = desired_velocity_xy.x; |
|
|
|
|
desired_velocity.y = desired_velocity_xy.y; |
|
|
|
|
desired_velocity_neu_cms.x = desired_velocity_xy_cms.x; |
|
|
|
|
desired_velocity_neu_cms.y = desired_velocity_xy_cms.y; |
|
|
|
|
|
|
|
|
|
// limit vertical desired_velocity to slow as we approach target (we use 1/2 of maximum deceleration for gentle slow down)
|
|
|
|
|
// limit vertical desired_velocity_neu_cms to slow as we approach target (we use 1/2 of maximum deceleration for gentle slow down)
|
|
|
|
|
const float des_vel_z_max = copter.avoid.get_max_speed(pos_control->get_pos_z_p().kP().get(), pos_control->get_accel_z() * 0.5f, fabsf(dist_vec_offs_neu.z), copter.G_Dt); |
|
|
|
|
desired_velocity.z = constrain_float(desired_velocity.z, -des_vel_z_max, des_vel_z_max); |
|
|
|
|
desired_velocity_neu_cms.z = constrain_float(desired_velocity_neu_cms.z, -des_vel_z_max, des_vel_z_max); |
|
|
|
|
|
|
|
|
|
// get avoidance adjusted climb rate
|
|
|
|
|
desired_velocity.z = get_avoidance_adjusted_climbrate(desired_velocity.z); |
|
|
|
|
desired_velocity_neu_cms.z = get_avoidance_adjusted_climbrate(desired_velocity_neu_cms.z); |
|
|
|
|
|
|
|
|
|
// calculate vehicle heading
|
|
|
|
|
switch (g2.follow.get_yaw_behave()) { |
|
|
|
@ -140,7 +140,7 @@ void Copter::ModeFollow::run()
@@ -140,7 +140,7 @@ void Copter::ModeFollow::run()
|
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
case AP_Follow::YAW_BEHAVE_DIR_OF_FLIGHT: { |
|
|
|
|
const Vector3f vel_vec(desired_velocity.x, desired_velocity.y, 0.0f); |
|
|
|
|
const Vector3f vel_vec(desired_velocity_neu_cms.x, desired_velocity_neu_cms.y, 0.0f); |
|
|
|
|
if (vel_vec.length() > 100.0f) { |
|
|
|
|
yaw_cd = get_bearing_cd(Vector3f(), vel_vec); |
|
|
|
|
use_yaw = true; |
|
|
|
@ -164,7 +164,7 @@ void Copter::ModeFollow::run()
@@ -164,7 +164,7 @@ void Copter::ModeFollow::run()
|
|
|
|
|
last_log_ms = now; |
|
|
|
|
} |
|
|
|
|
// re-use guided mode's velocity controller (takes NEU)
|
|
|
|
|
Copter::ModeGuided::set_velocity(desired_velocity, use_yaw, yaw_cd, false, 0.0f, false, log_request); |
|
|
|
|
Copter::ModeGuided::set_velocity(desired_velocity_neu_cms, use_yaw, yaw_cd, false, 0.0f, false, log_request); |
|
|
|
|
|
|
|
|
|
Copter::ModeGuided::run(); |
|
|
|
|
} |
|
|
|
|