Plane: move two functions out of landing.cpp

- these two functions will be hard to port to AP_Landing due to complex dependancies so we'll defer them by moving them ArduPlane.cpp
This commit is contained in:
Tom Pittenger 2016-11-16 17:24:51 -08:00 committed by Tom Pittenger
parent d2376b7c8b
commit 5dbb2d4c2a
2 changed files with 313 additions and 309 deletions

View File

@ -1045,4 +1045,51 @@ void Plane::update_optical_flow(void)
}
#endif
/*
If land_DisarmDelay is enabled (non-zero), check for a landing then auto-disarm after time expires
*/
void Plane::disarm_if_autoland_complete()
{
if (g.land_disarm_delay > 0 &&
landing.complete &&
!is_flying() &&
arming.arming_required() != AP_Arming::NO &&
arming.is_armed()) {
/* we have auto disarm enabled. See if enough time has passed */
if (millis() - auto_state.last_flying_ms >= g.land_disarm_delay*1000UL) {
if (disarm_motors()) {
gcs_send_text(MAV_SEVERITY_INFO,"Auto disarmed");
}
}
}
}
/*
the height above field elevation that we pass to TECS
*/
float Plane::tecs_hgt_afe(void)
{
/*
pass the height above field elevation as the height above
the ground when in landing, which means that TECS gets the
rangefinder information and thus can know when the flare is
coming.
*/
float hgt_afe;
if (flight_stage == AP_SpdHgtControl::FLIGHT_LAND_FINAL ||
flight_stage == AP_SpdHgtControl::FLIGHT_LAND_PREFLARE ||
flight_stage == AP_SpdHgtControl::FLIGHT_LAND_APPROACH) {
hgt_afe = height_above_target();
hgt_afe -= rangefinder_correction();
} else {
// when in normal flight we pass the hgt_afe as relative
// altitude to home
hgt_afe = relative_altitude();
}
return hgt_afe;
}
AP_HAL_MAIN_CALLBACKS(&plane);

View File

@ -135,25 +135,6 @@ bool Plane::verify_land()
return false;
}
/*
If land_DisarmDelay is enabled (non-zero), check for a landing then auto-disarm after time expires
*/
void Plane::disarm_if_autoland_complete()
{
if (g.land_disarm_delay > 0 &&
auto_state.land_complete &&
!is_flying() &&
arming.arming_required() != AP_Arming::NO &&
arming.is_armed()) {
/* we have auto disarm enabled. See if enough time has passed */
if (millis() - auto_state.last_flying_ms >= g.land_disarm_delay*1000UL) {
if (disarm_motors()) {
gcs_send_text(MAV_SEVERITY_INFO,"Auto disarmed");
}
}
}
}
void Plane::adjust_landing_slope_for_rangefinder_bump(void)
{
// check the rangefinder correction for a large change. When found, recalculate the glide slope. This is done by
@ -300,27 +281,3 @@ void Plane::setup_landing_glide_slope(void)
/*
the height above field elevation that we pass to TECS
*/
float Plane::tecs_hgt_afe(void)
{
/*
pass the height above field elevation as the height above
the ground when in landing, which means that TECS gets the
rangefinder information and thus can know when the flare is
coming.
*/
float hgt_afe;
if (flight_stage == AP_SpdHgtControl::FLIGHT_LAND_FINAL ||
flight_stage == AP_SpdHgtControl::FLIGHT_LAND_PREFLARE ||
flight_stage == AP_SpdHgtControl::FLIGHT_LAND_APPROACH) {
hgt_afe = height_above_target();
hgt_afe -= rangefinder_correction();
} else {
// when in normal flight we pass the hgt_afe as relative
// altitude to home
hgt_afe = relative_altitude();
}
return hgt_afe;
}