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refinement of alt hold and Hein's Yaw hold fix

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git-svn-id: https://arducopter.googlecode.com/svn/trunk@2377 f9c3cf11-9bcb-44bc-f272-b75c42450872
This commit is contained in:
jasonshort 2011-05-21 16:24:07 +00:00
parent b8d3b12b35
commit 16df94168f
1 changed files with 10 additions and 7 deletions
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17
ArduCopterMega/Attitude.pde
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@ -132,20 +132,22 @@ void calc_nav_throttle()
if(error < 0){
// try and prevent rapid fall
scaler = (altitude_sensor == BARO) ? .9 : .9;
scaler = (altitude_sensor == BARO) ? .5 : .9;
}
if(altitude_sensor == BARO){
nav_throttle = g.pid_baro_throttle.get_pid(error, delta_ms_fast_loop, scaler); // .25
nav_throttle = g.throttle_cruise + constrain(nav_throttle, -70, 140);
nav_throttle = g.pid_baro_throttle.get_pid(error, dTnav2, scaler); // .25
nav_throttle = g.throttle_cruise + constrain(nav_throttle, -50, 100);
}else{
nav_throttle = g.pid_sonar_throttle.get_pid(error, delta_ms_fast_loop, scaler); // .5
nav_throttle = g.pid_sonar_throttle.get_pid(error, dTnav2, scaler); // .5
nav_throttle = g.throttle_cruise + constrain(nav_throttle, -70, 150);
}
nav_throttle = (nav_throttle + nav_throttle_old) >> 1;
nav_throttle_old = nav_throttle;
// simple filtering
nav_throttle = (nav_throttle + nav_throttle_old) >> 1;
nav_throttle_old = nav_throttle;
// clear the new data flag
invalid_throttle = false;
//Serial.printf("nav_thr %d, scaler %2.2f ", nav_throttle, scaler);
@ -257,7 +259,8 @@ output_yaw_with_hold(boolean hold)
}else{
// RATE control
long error = ((long)g.rc_4.control_in * 6) - rate; // control is += 6000 * 6 = 36000
// Hein, 5/21/11
long error = ((long)g.rc_4.control_in * 6) - (rate * 3); // control is += 6000 * 6 = 36000
g.rc_4.servo_out = g.pid_acro_rate_yaw.get_pid(error, delta_ms_fast_loop, 1.0); // kP .07 * 36000 = 2520
yaw_debug = YAW_RATE; // 2
}