This article explains how to land Plane as part of a mission plan and includes information about how a landing can be safely aborted.
Configuring for Automatic Landing¶
Plane can automatically land an aircraft, as part of a mission plan.
To land the plane you need to add a NAV_LAND command to the end of your mission indicating the latitude, longitude and altitude of your desired touchdown point. In most cases, the altitude should be set to 0. During landing, the autopilot will shut down the throttle and hold the current heading when the plane reaches the flare point, controlled by the parameters described below.
The key parameters that control automatic landing are:
The meaning and recommended value of each of these parameters is described below.
Setting the Flare Point¶
The “flare” is the final stage of the landing when the autopilot cuts the throttle and raises the pitch, increasing drag and slowing the aircraft to sink onto the ground. The appropriate time to flare depends on the type of aircraft, and is controlled by the LAND_FLARE_ALT and LAND_FLARE_SEC parameters.
The primary control of the flare is the
This is the time in seconds before the aircraft would hit the ground if it continued with its current descent rate.
So if the plane is descending at 2 meters/second and you set the
LAND_FLARE_SEC to 3 then the aircraft would flare at an altitude of 6 meters above the ground.
By using a time to impact to control the flare the aircraft is able to flare at a higher altitude if it is descending quickly, and at a lower altitude if it is descending slowly. That helps ensure the flare is able to produce a smooth touchdown.
The second control is
That is an altitude above the ground in meters at which the aircraft will flare, regardless of its descent rate.
The appropriate values for these two parameters depends on how the autopilot is estimating its altitude above the ground.
If the autopilot has a good rangefinder (such as LIDAR) then you can safely choose quite small numbers, and flare close to the ground.
That will generally produce a better landing.
A value for
LAND_FLARE_SEC of 1.5 and
LAND_FLARE_ALT of 2 is a good place to start with a LiDAR.
If you are relying solely on a barometer for landing altitude then you will probably need higher values, to account for barometric error.
Controlling the glide slope¶
Another important factor in setting up the flare point is the glide slope. The glide slope is the ratio of the distance from the last waypoint to the landing point, and the height difference between the last waypoint and the landing point. For example, if the landing point is 300 meters from the last waypoint, and the last waypoint is 30 meters above the ground then the glide slope is 10%.
If the glide slope is too steep then the aircraft will not be able to flare in time to avoid crashing, plus the autopilot may not be able to keep the plane on the approach slope accurately. It is recommended that you start with a glide slope of at most 10%. What glide slope your plane can handle will depend on how well your pitch controller tuning is, how good your TECS tuning is, and the landing speed you ask for.
If you find your aircraft is not following the desired glide slope accurately then you should first check your pitch tuning in your logs, and ensure that the demanded and achieved pitch match within a couple of degrees during landing. If they don’t then look at the documentation on pitch tuning (or possibly re-run AUTOTUNE). If the demanded and achieved pitch do match then you should check your TECS logs to ensure that the demanded and achieved airspeed are matching during landing. Have a look at the TECS tuning patch for more information.
You should also be aware that many model aircraft can glide for long distances, and it may be that your requested glide slope and airspeed combination just isn’t achievable.
Automatic landing is greatly assisted by the use of an airspeed sensor. When using an airspeed sensor the landing approach speed (the speed coming down the glide slope) is controlled by the TECS_LAND_ARSPD parameter, in meters/second.
You need to choose a value for
TECS_LAND_ARSPD that is above the
stall speed of your aircraft, but low enough that the aircraft is able
to lose altitude and land in a reasonable distance. Note that as the
stall speed is dependent on the weight of your aircraft you will need to
adjust the landing speed if you change the aircraft’s weight
significantly (such as by adding batteries or a camera).
To further improve landing you can use a Pre-Flare to reduce airspeed
just before the flare. This is enabled by setting either
LAND_PF_ALT or LAND_PF_SEC
to either enter a pre-flare state at a fixed altitude or at an estimated
seconds to ground (given your current decent rate). Once the Pre-Flare
is triggered the desired airspeed becomes LAND_PF_ARSPD.
This value should be lower than
TECS_LAND_ARSPD but greater than the
stall speed. This is particularly useful where reverse thrust is
available. However, some aircraft can handle a stall landing so setting
this to a very low number (1) will tell the aircraft to bleed off as
much airspeed as possible before the flare.
Controlling the approach¶
During the landing approach the autopilot needs to balance the requested
airspeed (set by
TECS_LAND_ARSPD) and the requested glide slope and
landing position (set by the previous waypoint and final landing point).
The default configuration tries to balance these two demands equally,
but for some aircraft you may want to prioritize one over the other.
The priority of airspeed control versus height control is set using the
parameter. A value of 1 (the default) means a balance between the two. A
value closer to two gives a higher priority to airspeed and a value
closer to zero gives a higher priority to height control. For example,
if you are landing at a speed close to the stall speed you may wish to
place a high priority on the airspeed control. To do that you should set
TECS_LAND_SPDWGT to a value close to 2, such as 1.9.
If what you want in a landing is precision in the position where it
lands then you should set
TECS_LAND_SPDWGT to a low number, such as
0.2 or even 0.0. In that case the plane will still try to achieve the
target landing airspeed by using the throttle, but it will not try to
control airspeed with pitch.
If you are landing a glider (or any aircraft without a motor) then you
TECS_LAND_SPDWGT to 2.0, so that airspeed is the priority
and pitch will be used to control airspeed.
In most cases a value of -1 gives the best result. This special value will auto-adjust the value during the landing, scaling it from your normal TECS_SPDWEIGHT value down to zero at the point of landing. So up in the sky during approach you maintain good airspeed but by the time you land the emphasis is on a more accurate landing.
Controlling the flare¶
The final stage of the landing is called the “flare”. During the flare the aircraft tries to retain a course along the line between the last waypoint and the landing waypoint, and it controls its height solely using a target descent rate. Once the flare is started the throttle is “disabled” - set to some value between THR_MIN and zero.
The main job of the autopilot in the flare is to try to achieve the descent rate specified in the TECS_LAND_SINK parameter. That defaults to 0.25 meters/second, which is a reasonable touchdown vertical speed for most models. To achieve that speed the TECS controller uses pitch control only as the motor has been forced to zero.
LAND_PITCH_CD parameter sets the minimum pitch target in the
flare (in centi-degrees). This parameter is very airframe specific and
is designed to prevent the nose of the aircraft being too far down on
touchdown causing issues with damaging the landing gear or breaking a
propeller. For most aircraft this should be a small positive number
(such as 300, meaning 3 degrees), but for some belly landing aircraft a
small negative number can be good, to allow the nose to be kept down a
small amount to reduce the chance of stall if the flare happens too far
off the ground.
Note that the actual pitch of the aircraft can be quite a bit above
LAND_PITCH_CD as the TECS controller tries to control the descent
rate. The maximum pitch is controlled by the
parameter if it is non-zero, otherwise by the
TECS_LAND_DAMP parameter is a damping constant for the pitch
control during flare. A larger number will cause the pitch demand to change
more slowly. This parameter can be used to reduce issues with sudden
pitch changes when the flare happens.
After the Flare¶
After the plane flares it continues to navigate, but with zero throttle. The navigation direction is a line extrapolated forward through the landing point from the last waypoint. Note that the navigation roll will be limited to LEVEL_ROLL_LIMIT (which defaults to 5 degrees) to prevent wing strike, so if there is a significant cross-wind then it is likely that the aircraft will not be able to maintain the exact path.
If your aircraft is consistently landing long (which can happen for a
variety of reasons) then you can adjust
either force a stall (negative) or bring it down (positive). This value
will adjust your
TECS_LAND_SINK proportional to the distance from
the LAND point. This helps ensure you land in a reasonable distance from
the LAND point.
Possible causes of landing long include ground effect giving the aircraft more lift as it is close to the ground or simply the aircraft traveling very fast.
When the plane has stopped moving for LAND_DISARMDELAY seconds (default 20 seconds) it will disarm the motor. Optionally, you can disable servo movement once LAND_DISARMDELAY has triggered by setting LAND_THEN_NEUTRL.
Using a rangefinder¶
If you have fitted a rangefinder to your aircraft then you can use it for much more accurate landing control. To allow the rangefinder to be used for landing you need to set the RNGFND_LANDING parameter to 1.
When using a rangefinder for landing the altitude given by the rangefinder is used only in the landing approach and to determine the flare point, and is designed to allow the aircraft to more accurately follow the glide slope and to flare at the right time.
The effectiveness of a rangefinder can depend on the surface you are flying over, so it is a good idea to do some low passes in a flight mode such as FBWA first, then examine the logs to check that the rangefinder is working correctly.
Also note that if you have a longer range rangefinder then it is a very good idea to set the minimum range of the rangerfinder well above zero. For example, the PulsedLight Lidar has a typical range of over 40 meters, and when it gets false readings it tends to read ranges of less than 1 meter. And setting RNGFND1_MIN_CM to 150 , if its the first system rangefinder, will discard any rangerfinder readings below 1.5 meters, and will greatly improve the robustness of the Lidar for landing.
Improving the landing¶
The key to a good landing is the autopilot knowing how far off the ground it is. With the default setup the only sensor available to detect altitude is the barometer. Unfortunately barometers suffer from three main types of error:
- barometric drift due to changes in atmospheric pressure
- barometric drift due to changes in the temperature of the autopilot electronics
- barometric error due to local pressure changes from airflow around the barometer
The ideal setup for good automatic landing is to have a
Lidar. A Lidar can measure
the distance to the ground very accurately, and doesn’t suffer from
drift. If you have a Lidar installed you can enable its use for landing
If a Lidar isn’t fitted then there are a few things you can do to minimise barometric error problems with auto-land
- perform a barometer calibration after the electronics have warmed up. The easiest way to do this with a Pixhawk is to disarm the plane with the safety switch. When the plane is disarmed it assumes it is on the ground and will zero the barometer to the current pressure.
- try to prevent direct airflow over the autopilot that could cause speed related pressure changes
- fly shorter flights, allowing for less time for airpressure changes. Check your logs and see if the landing is happening at zero altitude consistently
With planes that belly land it can also work well to setup the landing
with a shallow pitch (in
LAND_PITCH_CD) and set a slightly higher
altitude to flare at. That will only work if your stall speed is low
enough that gliding for a while will work reliably.
Sometimes it is useful to trigger an automatic landing as part of an RTL (return to launch). To do this you need to do two things:
- add a DO_LAND_START mission item to your mission, just before the start of your landing sequence
- set the RTL_AUTOLAND parameter to 1 or 2
The way it works is that when the plane enters an RTL it checks to see
if the parameter RTL_AUTOLAND is set to 1 or 2. If it is then the
current mission is searched for a mission item of type DO_LAND_START.
If one is found then the plane will automatically enter AUTO mode and
land, starting at the part of the mission just after the
The exact behaviour depends on the
RTL_AUTOLAND=1then the plane will first RTL as normal, then when it starts circling the return point (home or a rally point) it will then switch to the AUTO mission after the
RTL_AUTOLAND=2then the plane will bypass the RTL completely and go straight to the landing sequence.
You can optionally include more than one
DO_LAND_START mission item
in your mission. If that is done then the latitude/longitude of the
DO_LAND_START mission items is used to choose which landing sequence
to use. The
DO_LAND_START closest to the current location is used.
This can be useful if you have multiple landing sequences for different
wind conditions or different areas.
How to abort an auto-landing¶
A landing-abort mechanism is provided to allow you to abort a landing sequence in a safe, controlled, and expected way. Custom abort behaviour can be pre-programmed as part of the mission or you can use the default abort mechanism. To enable this feature set param LAND_ABORT_THR=1.
There are three steps to this feature:
This section describes the abort behavior introduced in Plane 3.4.
Step 1) Abort land triggers¶
The are three ways to trigger an auto-landing abort. All of them will only work while in AUTO mode and currently executing a
LAND waypoint mission item:
- Send the ``MAV_CMD_DO_GO_AROUND`` command using a GCS. Mission Planner has a button labeled “Abort Landing” on the FlightData Actions tab.
- RC input Throttle > 90%. This will trigger an abort while staying in AUTO mode. The throttle only needs to be high briefly to trigger it. Don’t forget to lower it!
- Mode change. For human piloted landing abort you can switch out of AUTO mode into, for example MANUAL/STABILIZE/FBWA, and navigate the aircraft safely however you’d like. Using this method will skip abort behavior step 2 because it is being done manually. When switching back to AUTO the mission will resume as described in step 3 below.
Step 2) Abort land flight behavior¶
The abort behaviour has a default configuration and does not require a pre-planned mission. The default abort behavior is to simulate an auto-takeoff: pitch up at least 10 degrees and set throttle to TKOFF_THR_MAX and hold the heading until it reaches a target altitude of 30m. It is possible to override the pitch and altitude to allow for a customized behavior.
- Pitch minimum. If there was a NAV_TAKEOFF ever executed on this mission then the same pitch will be re-used here.
- Target altitude. If NAV_LAND param1 is >0 then it is used as a target altitude in meters. Else If a NAV_TAKEOFF was ever executed on this mission then the same altitude will be re-used here.
This step is skipped if the abort trigger is via mode change because it is assumed the pilot manually took over and flew the aircraft to a safe altitude at the pitch and throttle of their choosing.
Step 3) Mission state after an aborted landing completes¶
Once an abort land has completed, by either reaching the target altitude or switching back to AUTO, the mission index will have changed and you will no longer be executing a NAV_LAND command. The mission index will change to be one of these three options and checked for in this order:
- If the NAV_LAND mission item is followed by mission item CONTINUE_AND_CHANGE_ALT with param1 = 0 or 1 then the mission index will increment once to that command and execute it like normal. This can be followed by further post-abort mission planning for any custom planned mission behavior.
- Else If there is a DO_LAND_START in the mission then it jumps to that index.
- Else the mission index decrements once to be the index before the NAV_LAND. This will ensure the same landing approach is repeated.
Some ESC’s allow for reverse direction. When using reverse on the propeller it will generate a negative thrust which can be used to reduce your airspeed. During a steep landing approach this method can be used to maintain a stable and low airspeed allowing you to land much more softly and precisely. To use this feature it is highly recommend to use an airspeed sensor and a rangefinder (see above) for an accurate altitude.
Reverse-thrust landings are available starting from Plane v3.5.1.
The below video is an example of a Skywalker X8 performing an auto-landing with a 15 degree slope. The target is the hat on the ground showing it is possible to get repeatable high precision landings where the final position error was dictated by the GPS position error. This particular aircraft has been landed at 20deg and 25deg slopes too. YMMV depending on weight of aircraft and available thrust from motor/propeller. Typically a Skywalker X8 would need a shallow slope such at 6 to 10deg.
The key parameters that control reverse thrust landing in addition to the ones listed in section 1.1 are:
Most important is to set the :SERVO3_TRIM (assuming the esc/motor is attached to output 3)to the point that the ESC is idle, usually around mid-range (1500us) to create an output curve that has SERVO3_MAX for full forward thrust, and SERVO3_MIN for full reverse thrust. This should be done AFTER the RC Calibrations setup step. The maximum amount of reverse thrust used in autopilot throttle controlled modes is set by THR_MIN. A value of -100 provides the maximum, while -20 would provide 20% of maximum, and so on.
The USE_REV_THRUST parameter is a bit mask that allows the setting of when reverse thrust can be activated, as when autolanding, or in other throttle controlled modes.
RCx_OPTION auxiliary function has been set, then activating the switch will also provide access to the reverse thrust capability in non-throttle controlled modes, as shown in the figure below.
ESC (Electronic Speed Controller)¶
Hardware selection and programming¶
Many ESCs can operate in forwards and reverse, however that is usually not a stock feature and may need to be reprogrammed to do it. Any SimonK and BLHeli compatible ESC can be flashed to support reverse thrust.
Remove propeller while configuring ESCs and thrust parameters
Configure your ESC for reverse thrust by changing its neutral point. Many ESC require custom firmware to accomplish this. Search Google or your ESC’s mfgr for instructions on how to configure your particular ESC.
Set Minimum PWM to 1000, mid to 1500, and maximum to 2000, corresponding to maximum reverse thrust,idle, and maximum positive thrust from the ESC/Motor.
Determining your max glide slope angle¶
For a steep landing approach, the limitation is how well you can maintain your desired airspeed. This is determined by your aircraft’s ability to create reverse thrust (motor+prop thrust ability) and its resistance to slowing down (aircraft mass). In many cases extreme steepness is unnecessary, but possible. With an over-sized motor and lightweight aircraft you can come in as steep as 60 degrees.
To determine your steepest approach angle, set TECS_APPR_SMAX very high as to not limit you (e.g. 99). Next, plan a mission with a steeper than normal approach (try 15 degrees and go up from there). Watch your airspeed on the approach - the aircraft should be able to maintain TECS_LAND_ARSPD without exceeding 75% of the available reverse throttle range. If not, you’re coming in too steep for the negative-thrust-to-mass ratio of your aircraft.
Keep in mind that whatever value you determine as your maximum may not be acceptable in all wind conditions. It is best to be a little conservative to maintain repeatability.
Setting up the Pre-Flare¶
With a rangefinder and airspeed sensors installed, at the pre-flare point we will have an accurate airspeed and altitude reading.
This gives us a good idea of our momentum and stable “initial conditions” to the final flare.
LAND_PF_SEC) to a fairly high point (for example 10m) and adjust from there.
LAND_PF_ARSPD to a value just above your stall speed.
When LAND_PF_ALT is reached the airspeed demand will instantly go from TECS_LAND_ARSPD to LAND_PF_ARSPD. This will cause it to slam on the brakes via increased reverse thrust so that the airspeed reduces to the desired airspeed.
The trick is to set
LAND_PF_ALT to an altitude where it
LAND_PF_ARSPD before killing the throttle at
LAND_FLARE_ALT (which occurs at a somewhat low altitude - around 1
TECS_LAND_ARSPD = 15,
LAND_PF_ARSPD = 12,
Depending on your slope, mass of aircraft and motor+propeller thrust
ability, you’re expecting the aircraft to decelerate from 15m/s to 12m/s
airspeed while dropping 10m to 2m. These are the critical params to adjust to
ensure a smooth and slow flare below 2m altitude.
Now that you are starting the flare with a stable and predictable airspeed, it’s much easier to control the flare. If you’ve already tuned your flare for an auto-land without reverse thrust you’ll want to retune it. You’ll notice you’re coming in much slower ad tuning will be easier. The tweaks and compromises you had to do before are much easier to deal with.
Determining actual stall speed of your aircraft¶
Unless you really know what you’re doing, stall speed can be hard to estimate. Traditionally, to determine this true value you would need to slowly decrease your airspeed until you stall but that comes with the pesky problem that now you have a stalled aircraft falling out of the sky.
LAND_PF_ARSPD you can check your stall speed much lower to the ground.
To know the airspeed at the exact moment it stalls, check your dataflash logs (
*.bin on SD card) for the airspeed (ARSP.Airspeed) when your wing loses lift and drops by comparing actual roll (CTUN.Roll) and desired roll (CTUN.NavPitch) diverge.