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ArduCopter: fix heli build

This commit is contained in:
rmackay9 2012-10-06 13:46:19 +09:00
parent e33d314f1d
commit 05fd04134a
1 changed files with 12 additions and 18 deletions
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30
ArduCopter/Attitude.pde
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@ -14,8 +14,8 @@ get_stabilize_roll(int32_t target_angle)
// convert to desired Rate:
target_angle = g.pi_stabilize_roll.get_pi(target_angle, G_Dt);
// output control:
return constrain(target_angle, -4500, 4500);
// output control - we do not use rate controllers for helicopters so send directly to servos
g.rc_1.servo_out = constrain(target_angle, -4500, 4500);
#else
// convert to desired Rate:
@ -48,8 +48,8 @@ get_stabilize_pitch(int32_t target_angle)
// convert to desired Rate:
target_angle = g.pi_stabilize_pitch.get_pi(target_angle, G_Dt);
// output control:
return constrain(target_angle, -4500, 4500);
// output control - we do not use rate controllers for helicopters so send directly to servos
g.rc_2.servo_out = constrain(target_angle, -4500, 4500);
#else
// convert to desired Rate:
@ -93,12 +93,8 @@ get_stabilize_yaw(int32_t target_angle)
// do not use rate controllers for helicotpers with external gyros
#if FRAME_CONFIG == HELI_FRAME
if(!motors.ext_gyro_enabled) {
yaw_rate_target_ef = target_rate;
yaw_rate_trim_ef = i_term;
}else{
// TO-DO: fix this for helicopters which don't use rate controller
output = constrain((target_rate + i_term), -4500, 4500);
if(motors.ext_gyro_enabled) {
g.rc_4.servo_out = constrain((target_rate + i_term), -4500, 4500);
}
#endif
@ -227,18 +223,10 @@ get_acro_yaw(int32_t target_rate)
void
update_rate_contoller_targets()
{
static int16_t counter = 0;
// convert earth frame rates to body frame rates
roll_rate_target_bf = roll_rate_target_ef + sin_pitch * yaw_rate_target_ef;
pitch_rate_target_bf = cos_roll_x * pitch_rate_target_ef + sin_roll * yaw_rate_target_ef;
yaw_rate_target_bf = cos_pitch_x * cos_roll_x * yaw_rate_target_ef + sin_roll * pitch_rate_target_ef;
//counter++;
if( counter >= 100 ) {
counter = 0;
Serial.printf_P(PSTR("\nr:%ld\tp:%ld\ty:%ld\t"),ahrs.roll_sensor, ahrs.pitch_sensor, ahrs.yaw_sensor);
Serial.printf_P(PSTR("Rrate:%ld/%ld\tPrate:%ld/%ld\tYrate:%ld/%ld\n"),roll_rate_target_ef, roll_rate_target_bf, pitch_rate_target_ef, pitch_rate_target_bf, yaw_rate_target_ef, yaw_rate_target_bf);
}
}
// run roll, pitch and yaw rate controllers and send output to motors
@ -246,10 +234,16 @@ get_acro_yaw(int32_t target_rate)
void
run_rate_controllers()
{
#if FRAME_CONFIG == HELI_FRAME // helicopters only use rate controllers for yaw and only when not using an external gyro
if(!motors.ext_gyro_enabled) {
g.rc_4.servo_out = get_rate_yaw(yaw_rate_target_bf) + yaw_rate_trim_ef;
}
#else
// call rate controllers
g.rc_1.servo_out = get_rate_roll(roll_rate_target_bf) + roll_rate_trim_ef;
g.rc_2.servo_out = get_rate_pitch(pitch_rate_target_bf) + pitch_rate_trim_ef;
g.rc_4.servo_out = get_rate_yaw(yaw_rate_target_bf) + yaw_rate_trim_ef;
#endif
}
static int16_t