Flying a QuadPlane

While flying a QuadPlane can actually be easier than flying a conventional fixed wing aircraft there are some things you need to understand. Please read the following sections carefully.


QuadPlane transition is where the aircraft is changing between flying primarily as a VTOL (copter-like) aircraft and flying as a conventional fixed wing aircraft. Transition happens in both directions, and can either be commanded by the pilot or happen automatically based on airspeed/attitude/altitude(Assisted Fixed-Wing Flight) or flight mode changes during a mission.

The primary way to initiate a transition is to change flight mode, either using the flight mode channel on your transmitter or using a ground station to command a mode change.

During a transition, depending on type of QuadPlane and various Q_OPTIONS settings, pilot control of the vehicle’s attitude, climb rate, etc. may be modified or restricted to assure successful transition as detailed below.


See Tailsitter Section for details on transitions for tailsitters, which are different than non-tailsitters discussed below:

Transition to Fixed Wing Mode from VTOL

  • If you transition to MANUAL or ACRO, then the VTOL motors will immediately stop. In the case of a tilt-rotor, the motors will also immediately rotate to foward flight orientation.


If you do not have sufficient airspeed, an immediate stall will occur! Since MANUAL mode is often setup as a reflex driven “bail-out”, some users move, or remove this mode, and substitute QSTABLIZE or QLOITER as an alternative “bail-out” for a QuadPlane

  • If you transition to any other fixed wing mode then the VTOL motors will continue to supply lift and stability until you have reached the ARSPD_FBW_MIN airspeed (or airspeed estimate if no airspeed sensor). This phase is called “Transition airspeed wait”.
  • In non-tilt rotor configurations, the forward motor(s) thrust is controlled by the throttle stick in a manner similar to whatever fixed wing mode was entered. Transitioning to FBWB/CRUISE, throttle stick controls forward thrust as in that mode, as a speed or throttle value, depending on whether or not an airspeed sensor is in use. In FBWA/STABILIZE transitions, it is directly controlled, ie low stick is zero thrust and the QuadPlane will just hover. The VTOL motors will behave similar to that in QHOVER and will try to maintain present altitude throughout the transition. During the transition, elevator input will act as climb/descent demand to the VTOL motors, roll input as roll attitude change, unless Q_OPTIONS bit 0 is set.
  • In the case of tilt-rotors, the motors will tilt to Q_TILT_MAX for throttle stick positions at or above mid-stick to begin building forward airspeed for the transition. In FBWA/STABILIZE transitions, throttle stick positions below mid-stick will proportionately rotate VTOL motors back towards vertical, since that controls the forward thrust component. Transitioning to FBWB/CRUISE in any configuration, throttle stick has no effect until transition is complete. Overall thrust to the motors will behave similar to that in QHOVER and will try to maintain present altitude throughout the transition. During the transition, elevator input will act as climb/descent demand to the VTOL motors, roll input as roll attitude change, unless Q_OPTIONS bit 0 is set.


Unless the Q_OPTIONS bit 0 is set, pulling back on elevator will not only pitch the nose up but also increase the VTOL motor output to assist in climbing during the transition airspeed wait phase. If bit 0 is set, only the pitch will change and altitude will not. In tilt-rotors, this can lead to delaying, or even preventing, the transition from ever completing! For tilt-rotors, do not pull back on pitch if this bit is set, until the transition is completed!

  • Once ARSPD_FBW_MIN is reached the VTOL only motors’ contribution will slowly drop in power over Q_TRANSITION_MS milliseconds (default is 5000, so 5 seconds) and will switch off after that. And tilt-rotors will slowly rotate to full forward thrust configuration. Once transition is completed, normal control of throttle and attitude resumes for whatever fixed wing mode the vehicle is now in.


Usually by this time the VTOL motor contribution is already very low, since the QuadPlane is already flying, providing lift or climbing, and the VTOL contribution is only aiding attitude stabilization as required.

  • If Q_TRANS_FAIL is not zero, then exceeding this time before reaching ARSPD_FBW_MIN airspeed will cancel the transition and the aircraft will immediately change to QLAND. The default is 0, which disables this timeout.

Transition to a VTOL mode

If you transition from a fixed wing mode to a QuadPlane VTOL mode then the forward motor/thrust will immediately stop, and the control surfaces will continue to provide stability while the plane slows down. This allows for transitions to QuadPlane modes while flying at high speed. Tilt-rotors will, therefore, immediately move to VTOL position.

  • VTOL attitude control will be provided as needed as the vehicle slows.
  • Transition to altitude holding VTOL modes will manage power to the VTOL motors as necessary to hold altitude as the vehicle slows from forward fixed wing flight.
  • Transition to non-altitude holding VTOL modes will provide vertical thrust as commanded by the throttle.
  • Transition to QLOITER will project a stopping position to maintain based on deceleration of the vehicle and then hold it once reached.

The one exception to the forward motor stopping in QuadPlane VTOL modes is if you have the Q_VFWD_GAIN parameter set to a non-zero value. In that case the forward motor will be used to hold the aircraft position in a wind. See the description of Q_VFWD_GAIN.


During transitions from VTOL to fixed wing mode, all motors can be running at very high levels. Battery sag below minimum levels (3.0V/cell for LiPo batteries) and resulting battery damage is possible. Extreme cases may even result in a crash due to VTOL motor output being too low. This is especially true when using high capacity, low C rating flight batteries common for long duration setups. This can be managed somewhat with manual throttle control when manually transitioning, but in AUTO mode, a VTOL to fixed wing transition is currently done with THR_MAX on the forward motor until transition is complete, so very high currents can be experienced. Whether or not this will be an issue can be determined by examining the battery voltage during a manually initiated transition from the flight log. If too much voltage sag is seen, the best solutions are to use a higher C rating flight battery, or use separate batteries for forward motors and the VTOL motors, or to use BATT_WATT_MAX and other parameters to limit excessive current draw during transitions. (See Limiting Excessive Battery Power Draw )

Tailsitter Transitions

Tailsitter transitions are slightly different. See Tailsitter Section for details.

VTOL vs Fixed-Wing Level Trim

Often fixed wing “level” trim, which is the pitch attitude stabilization modes attempt to maintain, is set to be several degrees positive with respect to the wing chord line in order to provide lift while cruising. This is accomplished either by running the accelerometer calibration level position set in this attitude, or after by using the “Calibrate Level” button in Mission Planner or by adjusting TRIM_PITCH_CD parameter.

However, when in VTOL modes, this can result in the vehicle leaning “backward” a few degrees, building in a tendency to drift backwards. This can be eliminated by setting the Q_TRIM_PITCH parameter to correct this. This can also be used to correct minor CG imbalances caused by VTOL motor placement not being exactly balanced around the CG.

Assisted Fixed-Wing Flight

The QuadPlane code can also be configured to provide assistance to the fixed wing code in any flight mode except MANUAL or ACRO. To enable quad assistance you should set Q_ASSIST_SPEED parameter to the airspeed below which you want assistance.

When Q_ASSIST_SPEED is non-zero then the quad motors will assist with both stability and lift whenever the airspeed drops below that threshold. This can be used to allow flying at very low speeds in FBWA mode for example, or for assisted automatic fixed wing takeoffs.


If you are not using an airspeed sensor, airspeed will be determined by the synthetic airspeed generated internally as a backup in case of airspeed sensor failure. This estimate can be very inaccurate at times. You may want to consider not enabling Assisted Fixed Wing Flight if not using an airspeed sensor to prevent false activations when airspeed really is above the threshold, but is being misrepresented by the internal airspeed.

It is suggested that you do initial flights with Q_ASSIST_SPEED set to zero just to test the basic functionality and tune the airframe. Then try with Q_ASSIST_SPEED above plane stall speed if you want that functionality.

From the 3.7.0 release an additional assistance type is available based on attitude error. If Q_ASSIST_ANGLE is non-zero then this parameter gives an attitude error in degrees above which assistance will be enabled even if the airspeed is above Q_ASSIST_SPEED. The attitude assistance will only be used if Q_ASSIST_SPEED greater than zero.

And as of Plane-4.0 and later, a third trigger to provide assistance is Q_ASSIST_ALT . This is the altitude below which QuadPlane assistance will be triggered. This acts the same way as Q_ASSIST_ANGLE and Q_ASSIST_SPEED, but triggers if the aircraft drops below the given altitude while the VTOL motors are not running. A value of zero disables this feature. The altutude is calculated as being above ground level. The height above ground is given from a Lidar used if available and RNGFND_LANDING =1 or from terrain data if TERRAIN_FOLLOW =1, or comes from height above home otherwise.

What assistance the quad motors provides depends on the fixed wing flight mode. If you are flying in an autonomous or semi-autonomous mode then the quad motors will try to assist with whatever climb rate and turn rate the autonomous flight mode wants when assistance is enabled (ie. airspeed is below Q_ASSIST_SPEED or attitude error is above Q_ASSIST_ANGLE , or altitude is below Q_ASSIST_ALT ). In a manually navigated mode the quad will try to provide assistance that fits with the pilot inputs.

The specific handling is:

  • In AUTO mode the quad will provide lift to get to the altitude of the next waypoint, and will help turn the aircraft at the rate the navigation controller is demanding.
  • In fixed wing LOITER, RTL or GUIDED modes the quad motors will try to assist with whatever climb rate and turn rate the navigation controller is asking for.
  • In CRUISE or FBWB mode the quad will provide lift according to the pilots demanded climb rate (controlled with pitch stick). The quad motors will try to turn at the pilot demanded turn rate (combining aileron and rudder input).
  • In FBWA mode the quad will assume that pitch stick input is proportional to the climb rate the user wants. So if the user pulls back on the pitch stick the quad motors will try to climb, and if the user pushes forward on the pitch stick the quad motors will try to provide a stable descent.
  • In AUTOTUNE mode the quad will provide the same assistance as in FBWA, but it is not a good idea to use AUTOTUNE mode with a high value of Q_ASSIST_SPEED as the quad assistance will interfere with the learning of the fixed wing gains.
  • In MANUAL, ACRO and TRAINING modes the quad motors will completely turn off. In those modes the aircraft will fly purely as a fixed wing.
  • In STABILIZE mode the quad motors will try to provide lift if assistance is turned on.

Return to Launch (RTL)

When flying a QuadPlane you have a choice of several methods of handling return to launch. The choices are:

  • circle about the return point as a fixed wing
  • fly as a VTOL aircraft to the return point then land vertically
  • fly as a fixed wing aircraft until close to the return point then switch to VTOL and land vertically

In each case a key concept is the return point. This is defined as the closest rally point, or if a rally point is not defined then the home location. See the Rally Points page for more information on rally points.

Fixed Wing RTL

The default behaviour of the RTL mode is the same as for fixed wing. It will fly to the nearest rally point (or home if no rally point is defined) and circle as a fixed wing aircraft about that point. The VTOL motors will not be used unless the aircraft drops below the airspeed defined in Q_ASSIST_SPEED. The altitude the aircraft will circle at will be the altitude in the rally point, or the ALT_HOLD_RTL altitude if a rally point is not being used.


If you prefer to do return to launch as a VTOL aircraft (like a multirotor would do) then you can use the QRTL flight mode. That flight mode will transition to VTOL flight and then fly at the Q_WP_SPEED speed towards the return point, at an altitude of Q_RTL_ALT.

Once the return point is reached the aircraft will start a vertical descent towards the ground for landing. The initial descent rate is set by Q_WP_SPEED_DN. Once the aircraft reaches an altitude of Q_LAND_FINAL_ALT the descent rate will change to Q_LAND_SPEED for the final landing phase.

In the final landing phase the aircraft will detect landing by looking for when the VTOL motor throttle drops below a minimum threshold for 5 seconds. When that happens the aircraft will disarm and the VTOL motors will stop.

Hybrid RTL

The final option for RTL in a QuadPlane is to fly as a fixed wing aircraft until it is close to the return point at which time it switches to a VTOL RTL as described above. To enable this type of hybrid RTL mode you need to set the Q_RTL_MODE parameter to 1.

The initial altitude that will be aimed for in the fixed wing portion of the hybrid RTL is the same as for a fixed wing RTL. You should set your rally point altitude and ALT_HOLD_RTL options appropriately to ensure that the aircraft arrives at a reasonable altitude for a vertical landing. A landing approach altitude of about 15 meters is good for many QuadPlanes. This should be greater than or equal to the Q_RTL_ALT values.

The distance from the return point at which the aircraft switches from fixed wing to VTOL flight is set using the RTL_RADIUS parameter, or if that is not set then the WP_LOITER_RAD parameter is used. The aircraft will then slow down as it approaches the return point, aiming for an altitude set by Q_RTL_ALT.

Once the return point is reached the aircraft begins to descend and land, exactly as described in the VTOL RTL mode above.

What Will Happen?

Understanding hybrid aircraft can be difficult at first, so below are some scenarios and how the ArduPilot code will handle them.

I am hovering in QHOVER/QLOITER and switch to FBWA mode

The aircraft will continue to hover, setting forward thrust/throttle at whatever the throttle stick position dictates and gaining speed. If you zero throttle during the transition, the aircraft will continue to hold the current height and hold itself level, slowing to a halt. It will drift with the wind as it is not doing position hold.

If you advance the throttle stick then the forward motor will throttle-up and the aircraft will start to move forward. The quad motors will continue to provide both lift and stability while the aircraft is moving slowly. You can control the attitude of the aircraft with roll and pitch stick input. When you use the pitch stick (elevator) that will affect the climb rate of the quad motors. If you pull back on the elevator the quad motors will assist with the aircraft climb. If you push forward on the pitch stick the power to the quad motors will decrease and the aircraft will descend.

The roll and pitch input also controls the attitude of the aircraft, so a right roll at low speed will cause the aircraft to move to the right. It will also cause the aircraft to yaw to the right (as the QuadPlane code interprets right aileron in fixed wing mode as a commanded turn).

Once the aircraft reaches an airspeed of ARSPD_FBW_MIN (or Q_ASSIST_SPEED if that is set and is greater than ARSPD_FBW_MIN) the amount of assistance the quad motors provide will decrease over 5 seconds. After that time the aircraft will be flying purely as a fixed wing.

I am flying fast in FBWA mode and switch to QHOVER mode

The quad motors will immediately engage and will start by holding the aircraft at the current height. The climb/descent rate is now set by the throttle stick, with a higher throttle stick meaning climb and a lower throttle stick meaning descend. At mid-stick the aircraft will hold altitude.

The forward motor will stop, but the aircraft will continue to move forward due to its momentum. The drag of the air will slowly bring it to a stop. The attitude of the aircraft can be controlled with roll and pitch sticks (aileron and elevator). You can yaw the aircraft with rudder.

I switch to RTL mode while hovering

The aircraft will transition to fixed wing flight. The quad motors will provide assistance with lift and attitude while the forward motor starts to pull the aircraft forward.

The normal Plane RTL flight plan will then be run, which defaults to circling at the RTL altitude above the arming position or nearest rally point. If you have RTL_AUTOLAND setup then the aircraft will do a fixed wing landing.

If you set Q_RTL_MODE to 1 then the aircraft will switch to a VTOL landing when it gets close to return point.

Radio or Throttle Failsafe

If flying in a plane mode or AUTO, behaviour is determined by the FS_SHORT_ACTN and FS_LONG_ACTN parameter settings (see Plane Failsafe Function). Quadplanes can be set such that instead of normal plane behviour on Failsafe induced RTLs, to transistion to QRTL and land once at the rally point or home, if Q_RTL_MODE =1. If not flying a mission, and are flying in any copter mode (QHOVER,QSTAB,etc.), failsafe will evoke QLAND or QRTL, depending on how Q_OPTIONS, bit 5, is set.

Typical Flight

A typical test flight would be:

  • VTOL takeoff in QLOITER or QHOVER
  • switch to FBWA mode and advance throttle over 50% and start flying fixed wing
  • switch to QHOVER mode to go back to quad mode and reduce throttle back to 50% for hover.