tecs msg: changed flight_path_angle to height rate as clearly we are

looking at height rates

Signed-off-by: Roman <bapstroman@gmail.com>
This commit is contained in:
Roman
2018-09-17 16:03:26 +02:00
committed by Daniel Agar
parent dd63a634b2
commit e17f0802cc
3 changed files with 6 additions and 6 deletions
+2 -2
View File
@@ -10,8 +10,8 @@ uint8 TECS_MODE_CLIMBOUT = 6
float32 altitude_sp
float32 altitude_filtered
float32 flight_path_angle_sp
float32 flight_path_angle
float32 height_rate_setpoint
float32 height_rate
float32 airspeed_sp
float32 airspeed_filtered
float32 airspeed_derivative_sp
@@ -568,8 +568,8 @@ FixedwingPositionControl::tecs_status_publish()
t.airspeed_sp = _tecs.TAS_setpoint_adj();
t.airspeed_filtered = _tecs.tas_state();
t.flight_path_angle_sp = _tecs.hgt_rate_setpoint();
t.flight_path_angle = _tecs.vert_vel_state();
t.height_rate_setpoint = _tecs.hgt_rate_setpoint();
t.height_rate = _tecs.vert_vel_state();
t.airspeed_derivative_sp = _tecs.TAS_rate_setpoint();
t.airspeed_derivative = _tecs.speed_derivative();
+2 -2
View File
@@ -210,8 +210,8 @@ void VtolType::check_quadchute_condition()
// We use tecs for tracking in FW and local_pos_sp during transitions
if (_tecs_running) {
// 1 second rolling average
_ra_hrate = (49 * _ra_hrate + _tecs_status->flight_path_angle) / 50;
_ra_hrate_sp = (49 * _ra_hrate_sp + _tecs_status->flight_path_angle_sp) / 50;
_ra_hrate = (49 * _ra_hrate + _tecs_status->height_rate) / 50;
_ra_hrate_sp = (49 * _ra_hrate_sp + _tecs_status->height_rate_setpoint) / 50;
// are we dropping while requesting significant ascend?
if (((_tecs_status->altitude_sp - _tecs_status->altitude_filtered) > _params->fw_alt_err) &&