Sub: Set EK2_ALT_NOISE on startup according to baro sensors detected.

This commit is contained in:
jaxxzer 2016-01-23 22:20:07 -05:00
parent a19fe0ded1
commit 20e29b6b3a
5 changed files with 60 additions and 5 deletions

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@ -24,7 +24,7 @@ void Sub::update_land_and_crash_detectors()
// called at MAIN_LOOP_RATE
void Sub::update_land_detector()
{
if(barometer.num_instances() > 1 && barometer.get_altitude() > SURFACE_END_DEPTH && ap.throttle_zero) {
if(barometer.num_instances() > 1 && barometer.get_altitude() > LAND_END_DEPTH && ap.throttle_zero) {
set_land_complete(true);
} else {
set_land_complete(false);
@ -46,3 +46,50 @@ void Sub::set_land_complete(bool b)
}
ap.land_complete = b;
}
// update_throttle_thr_mix - sets motors throttle_low_comp value depending upon vehicle state
// low values favour pilot/autopilot throttle over attitude control, high values favour attitude control over throttle
// has no effect when throttle is above hover throttle
void Sub::update_throttle_thr_mix()
{
#if FRAME_CONFIG != HELI_FRAME
// if disarmed or landed prioritise throttle
if(!motors.armed() || ap.land_complete) {
motors.set_throttle_mix_min();
return;
}
if (mode_has_manual_throttle(control_mode)) {
// manual throttle
if(channel_throttle->control_in <= 0) {
motors.set_throttle_mix_min();
} else {
motors.set_throttle_mix_mid();
}
} else {
// autopilot controlled throttle
// check for aggressive flight requests - requested roll or pitch angle below 15 degrees
const Vector3f angle_target = attitude_control.get_att_target_euler_cd();
bool large_angle_request = (pythagorous2(angle_target.x, angle_target.y) > 1500.0f);
// check for large external disturbance - angle error over 30 degrees
const Vector3f angle_error = attitude_control.get_att_error_rot_vec_cd();
bool large_angle_error = (pythagorous2(angle_error.x, angle_error.y) > 3000.0f);
// check for large acceleration - falling or high turbulence
Vector3f accel_ef = ahrs.get_accel_ef_blended();
accel_ef.z += GRAVITY_MSS;
bool accel_moving = (accel_ef.length() > 3.0f);
// check for requested decent
bool descent_not_demanded = pos_control.get_desired_velocity().z >= 0.0f;
if ( large_angle_request || large_angle_error || accel_moving || descent_not_demanded) {
motors.set_throttle_mix_max();
} else {
motors.set_throttle_mix_min();
}
}
#endif
}

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@ -233,8 +233,8 @@ void Sub::init_disarm_motors()
#endif
// we are not in the air
set_land_complete(true);
set_land_complete_maybe(true);
// set_land_complete(true);// We will let the land detector decide this in sub
// set_land_complete_maybe(true);
// log disarm to the dataflash
Log_Write_Event(DATA_DISARMED);

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@ -249,6 +249,11 @@ void Sub::init_ardupilot()
}
barometer.set_primary_baro(1); //Set the primary baro to external MS58XX
EKF.set_baro_alt_noise(0.1f);
EKF2.set_baro_alt_noise(0.1f);
} else { //We only have onboard baro
EKF.set_baro_alt_noise(10.0f);
EKF2.set_baro_alt_noise(10.0f);
}
// read Baro pressure at ground
//-----------------------------
@ -273,8 +278,7 @@ void Sub::init_ardupilot()
startup_INS_ground();
// set landed flags
set_land_complete(true);
set_land_complete_maybe(true);
set_land_complete(false);
// we don't want writes to the serial port to cause us to pause
// mid-flight, so set the serial ports non-blocking once we are

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@ -256,6 +256,8 @@ public:
// report any reason for why the backend is refusing to initialise
const char *prearm_failure_reason(void) const;
void set_baro_alt_noise(float noise) { _baroAltNoise.set_and_save(noise); };
static const struct AP_Param::GroupInfo var_info[];
private:

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@ -264,6 +264,8 @@ public:
// report any reason for why the backend is refusing to initialise
const char *prearm_failure_reason(void) const;
void set_baro_alt_noise(float noise) { _baroAltNoise.set_and_save(noise); };
// allow the enable flag to be set by Replay
void set_enable(bool enable) { _enable.set(enable); }