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Copter: roll-pitch fix to allow I to reduce

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Contributed by Leonard Hall
This commit is contained in:
Randy Mackay 2013-07-10 15:12:04 +09:00
parent d11e5497a4
commit 352a25e53f
1 changed files with 13 additions and 9 deletions
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22
ArduCopter/Attitude.pde
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@ -443,11 +443,12 @@ get_rate_roll(int32_t target_rate)
rate_error = target_rate - current_rate;
p = g.pid_rate_roll.get_p(rate_error);
// freeze I term if we've breached roll-pitch limits
if( motors.reached_limit(AP_MOTOR_ROLLPITCH_LIMIT) ) {
i = g.pid_rate_roll.get_integrator();
}else{
i = g.pid_rate_roll.get_i(rate_error, G_Dt);
// get i term
i = g.pid_rate_roll.get_integrator();
// update i term as long as we haven't breached the limits or the I term will certainly reduce
if (!motors.reached_limit(AP_MOTOR_ROLLPITCH_LIMIT) || ((i>0&&rate_error<0)||(i<0&&rate_error>0))) {
i = g.pid_rate_roll.get_i(rate_error, G_Dt);
}
d = g.pid_rate_roll.get_d(rate_error, G_Dt);
@ -485,12 +486,15 @@ get_rate_pitch(int32_t target_rate)
// call pid controller
rate_error = target_rate - current_rate;
p = g.pid_rate_pitch.get_p(rate_error);
// freeze I term if we've breached roll-pitch limits
if( motors.reached_limit(AP_MOTOR_ROLLPITCH_LIMIT) ) {
i = g.pid_rate_pitch.get_integrator();
}else{
// get i term
i = g.pid_rate_pitch.get_integrator();
// update i term as long as we haven't breached the limits or the I term will certainly reduce
if (!motors.reached_limit(AP_MOTOR_ROLLPITCH_LIMIT) || ((i>0&&rate_error<0)||(i<0&&rate_error>0))) {
i = g.pid_rate_pitch.get_i(rate_error, G_Dt);
}
d = g.pid_rate_pitch.get_d(rate_error, G_Dt);
output = p + i + d;