mirror of https://github.com/ArduPilot/ardupilot
Changed "rate" var to float from long.
git-svn-id: https://arducopter.googlecode.com/svn/trunk@1476 f9c3cf11-9bcb-44bc-f272-b75c42450872
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@ -4,8 +4,11 @@ void init_pids()
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// create limits to how much dampening we'll allow
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// this creates symmetry with the P gain value preventing oscillations
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max_stabilize_dampener = pid_stabilize_roll.kP() * 2500; // = 0.6 * 2500 = 1500 or 15°
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max_yaw_dampener = pid_yaw.kP() * 6000; // .5 * 6000 = 3000
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max_stabilize_dampener = pid_stabilize_roll.kP() * 2500; // = 0.6 * 2500 = 1500 or 15°
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//max_stabilize_dampener += pid_stabilize_roll.imax(); // = 0.1 * 300 = 1500 or 15°
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max_yaw_dampener = pid_yaw.kP() * 6000; // = .5 * 6000 = 3000
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//max_yaw_dampener += pid_yaw.imax(); // = 0.6 * 2500 = 1500 or 15°
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}
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@ -13,7 +16,7 @@ void output_stabilize()
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{
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float roll_error, pitch_error;
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Vector3f omega = dcm.get_gyro();
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long rate;
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float rate;
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int dampener;
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// control +- 45° is mixed with the navigation request by the Autopilot
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@ -37,12 +40,12 @@ void output_stabilize()
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// omega is the raw gyro reading
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// Limit dampening to be equal to propotional term for symmetry
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rate = degrees(omega.x) * 100; // 6rad = 34377
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dampener = ((float)rate * stabilize_dampener); // 34377 * .175 = 6000
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rate = degrees(omega.x) * 100.0; // 6rad = 34377
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dampener = (rate * stabilize_dampener); // 34377 * .175 = 6000
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rc_1.servo_out -= constrain(dampener, -max_stabilize_dampener, max_stabilize_dampener); // limit to 1500 based on kP
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rate = degrees(omega.y) * 100; // 6rad = 34377
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dampener = ((float)rate * stabilize_dampener); // 34377 * .175 = 6000
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rate = degrees(omega.y) * 100.0; // 6rad = 34377
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dampener = (rate * stabilize_dampener); // 34377 * .175 = 6000
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rc_2.servo_out -= constrain(dampener, -max_stabilize_dampener, max_stabilize_dampener); // limit to 1500 based on kP
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}
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@ -86,7 +89,9 @@ void output_yaw_with_hold(boolean hold)
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}
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if(hold){
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yaw_error = nav_yaw - yaw_sensor; // +- 60°
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// try and hold the current nav_yaw setting
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yaw_error = nav_yaw - yaw_sensor; // +- 60°
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yaw_error = wrap_180(yaw_error);
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// limit the error we're feeding to the PID
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@ -96,15 +101,15 @@ void output_yaw_with_hold(boolean hold)
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rc_4.servo_out = pid_yaw.get_pid(yaw_error, deltaMiliSeconds, 1.0); // .5 * 6000 = 3000
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// We adjust the output by the rate of rotation
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long rate = degrees(omega.z) * 100; // 3rad = 17188 , 6rad = 34377
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long rate = degrees(omega.z) * 100.0; // 3rad = 17188 , 6rad = 34377
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int dampener = ((float)rate * hold_yaw_dampener); // 18000 * .17 = 3000
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// Limit dampening to be equal to propotional term for symmetry
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rc_4.servo_out -= constrain(dampener, -max_yaw_dampener, max_yaw_dampener); // -3000
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}else{
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// rate control
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// rate control
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long rate = degrees(omega.z) * 100; // 3rad = 17188 , 6rad = 34377
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rate = constrain(rate, -36000, 36000); // limit to something fun!
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long error = ((long)rc_4.control_in * 6) - rate; // control is += 6000 * 6 = 36000
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@ -146,7 +151,8 @@ void output_rate_control()
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void reset_I(void)
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{
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pid_nav.reset_I();
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pid_throttle.reset_I();
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pid_baro_throttle.reset_I();
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pid_sonar_throttle.reset_I();
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}
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