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TradHeli - Attitude.pde - made yaw contol use jason's stability patch 

Quad - fixed small bug in pitch control (was using roll's stabilise controller)
This commit is contained in:
Randy Mackay 2011-12-08 22:23:50 +09:00
parent ee8986c463
commit ced26d7ba2
1 changed files with 12 additions and 15 deletions
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27
ArduCopter/Attitude.pde
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@ -66,7 +66,7 @@ get_stabilize_pitch(int32_t target_angle)
rate = g.pi_stabilize_pitch.get_p(error);
// experiment to pipe iterm directly into the output
int16_t iterm = g.pi_stabilize_roll.get_i(error, G_Dt);
int16_t iterm = g.pi_stabilize_pitch.get_i(error, G_Dt);
error = rate - (omega.y * DEGX100);
rate = g.pi_rate_pitch.get_pi(error, G_Dt);
@ -91,31 +91,28 @@ get_stabilize_yaw(int32_t target_angle)
// limit the error we're feeding to the PID
error = constrain(error, -YAW_ERROR_MAX, YAW_ERROR_MAX);
#if FRAME_CONFIG == HELI_FRAME // cannot use rate control for helicopters
// convert to desired Rate:
rate = g.pi_stabilize_yaw.get_pi(error, G_Dt);
if(!g.heli_ext_gyro_enabled ) {
error = rate - (degrees(omega.z) * 100.0);
rate = g.pi_rate_yaw.get_pi(error, G_Dt);
}
// output control:
rate = constrain(rate, -4500, 4500);
return (int)rate;
#else
// convert to desired Rate:
rate = g.pi_stabilize_yaw.get_p(error);
// experiment to pipe iterm directly into the output
int16_t iterm = g.pi_stabilize_yaw.get_i(error, G_Dt);
error = rate - (omega.z * DEGX100);;
#if FRAME_CONFIG == HELI_FRAME // cannot use rate control for helicopters
if( !g.heli_ext_gyro_enabled ) {
error = rate - (omega.z * DEGX100);
rate = g.pi_rate_yaw.get_pi(error, G_Dt);
}
// output control:
rate = constrain(rate, -4500, 4500);
#else
error = rate - (omega.z * DEGX100);
rate = g.pi_rate_yaw.get_pi(error, G_Dt);
// output control:
rate = constrain(rate, -2500, 2500);
return (int)rate + iterm;
#endif
return (int)rate + iterm;
}
#define ALT_ERROR_MAX 300