mirror of https://github.com/ArduPilot/ardupilot
AP_TECS: ensure good TECS state before running update_pitch_throttle
update_pitch_throttle can be called when update_50hz hasn't run in a very long time, or ever. This requires a main loop rate >50Hz, and for the mode change to occur in the same loop that update_50Hz doesn't run but update_pitch_throttle does.
This commit is contained in:
parent
94201f12c6
commit
99012bd525
|
@ -1155,8 +1155,18 @@ void AP_TECS::update_pitch_throttle(int32_t hgt_dem_cm,
|
|||
float hgt_afe,
|
||||
float load_factor)
|
||||
{
|
||||
// Calculate time in seconds since last update
|
||||
uint64_t now = AP_HAL::micros64();
|
||||
// check how long since we last did the 50Hz update; do nothing in
|
||||
// this loop if that hasn't run for some signficant period of
|
||||
// time. Notably, it may never have run, leaving _TAS_state as
|
||||
// zero and subsequently division-by-zero errors.
|
||||
const float _DT_for_update_50hz = (now - _update_50hz_last_usec) * 1.0e-6f;
|
||||
if (_update_50hz_last_usec == 0 || _DT_for_update_50hz > 1.0) {
|
||||
// more than 1 second since it was run, don't do anything yet:
|
||||
return;
|
||||
}
|
||||
|
||||
// Calculate time in seconds since last update
|
||||
_DT = (now - _update_pitch_throttle_last_usec) * 1.0e-6f;
|
||||
_DT = MAX(_DT, 0.001f);
|
||||
_update_pitch_throttle_last_usec = now;
|
||||
|
|
Loading…
Reference in New Issue