Advanced Tuning


this page has been superseded and is now ARCHIVED.

This article provides an overview of how to tune various Copter parameters.


The default PID gains are meant for the 3DR IRIS although they work on a wide variety of frames. Still, to get optimal performance you may need to adjust them which can be done through the Mission Planner’s Config/Tuning | Copter Pids screen. The screen shot below shows the most important parameters for Roll/Pitch (yellow), Yaw (orange), Altitude hold (green), Loiter (pink) and Waypoint navigation (blue).


The most important parameter to get right is the Rate Roll P (and by default Rate Pitch P is locked to the same value) as discussed here.

Normally it’s best to start by tuning the Rate Roll/Pitch P in Stabilize mode then move onto tuning altitude hold in AltHold mode, then Loiter (which often needs no tuning) and finally the waypoint navigation performance in Auto mode.


Dave C’s AC2.8.1 tuning guide has good information for tuning for rate roll and pitch but altitude hold, Loiter and navigation has changed dramatically since AC2.8.1 so those sections are no longer valid.

Roll/Pitch tuning

The Stabilize Roll/Pitch and Rate Roll/Pitch parameters, highlighted in yellow in the screen shot above control the roll pitch response.

The Rate parameters which convert the desired rotation rate into a motor output are the most important. The Rate Roll and Pitch P tuning page has the most information on tuning them.

The Stabilize Roll/Pitch P converts the desired angle into a desired rotation rate which is then fed to the Rate controller.

  • A higher value will make the copter more responsive to roll/pitch inputs, a lower value will make it smoother

  • If set too high, the copter will oscillate on the roll and/or pitch axis

  • If set too low the copter will become sluggish to inputs

More information on tuning the roll and pitch can be found on the Stabilize mode page’s Tuning section.

An objective view of the overall Roll and Pitch performance can be seen by graphing the dataflash log’s ATT message’s Roll-In vs Roll and Pitch-In vs Pitch. The “Roll” (i.e. actual roll) should closely follow the “Roll-In” while in Stabilize or AltHold modes. Pitch should similarly closely follow Pitch-In.

Alternatively you may wish to try tuning both the rate and stabilize (i.e. angular) parameters using the AutoTune feature.

Yaw tuning

The Stabilize Yaw and Rate Yaw parameters, highlighted in orange in the screen shot above control the yaw response. It’s rare that the yaw requires much tuning.

Similar to roll and pitch if either Stabilize Yaw P or Rate Yaw P is too high the copter’s heading will oscillate. If they are too low the copter may be unable to maintain its heading.

As mentioned on the Stabilize mode’s tuning section, the ACRO_Y_RATE parameter controls how quickly copter rotates based on a pilot’s yaw input. The default of 4.5 commands a 200 deg/sec rate of rotation when the yaw stick is held fully left or right. Higher values will make it rotate more quickly.

Altitude Tuning

The Altitude hold related tuning parameters are highlighted in green in the screen shot above.

The Altitude Hold P is used to convert the altitude error (the difference between the desired altitude and the actual altitude) to a desired climb or descent rate. A higher rate will make it more aggressively attempt to maintain its altitude but if set too high leads to a jerky throttle response.

The Throttle Rate (which normally requires no tuning) converts the desired climb or descent rate into a desired acceleration up or down.

The Throttle Accel PID gains convert the acceleration error (i.e the difference between the desired acceleration and the actual acceleration) into a motor output. The 1:2 ratio of P to I (i.e. I is twice the size of P) should be maintained if you modify these parameters. These values should never be increased but for very powerful copters you may get better response by reducing both by 50% (i.e P to 0.5, I to 1.0).

See the Altitude Hold flight mode page for more information.

Loiter Tuning

Generally if Roll and Pitch are tuned correctly, the GPS and compass are set-up and performing well and vibration levels are acceptable, Loiter does not require much tuning but please see the Loiter Mode page for more details on tunable parameters including the horizontal speed.

In-flight tuning

See the Transmitter based tuning page for details.

Filter tuning

Copters are often affected by vibration and tuning the various software filters available is critical to achieving an overall tune. A guide on tuning the various notch filters available can be found on the Notch Filtering wiki page.

Video introduction to PIDs

PIDs (Proportional - Integral - Derivative) are the method used by our firmware to continuously stabilize the vehicle

  • Proportional = Immediate Correction: The further off you are the bigger the correction you make.

  • Integral = Over time or steady state correction: If we are failing to make progress add additional correction.

  • Derivative = Take it Easy correction: Is the correction going to fast? if it is slow it down (dampen) it a bit to avoid overshoot.