Refer to this page if you’re using version 4.1.
The autonomous soaring functionality in ArduPilot allows the plane to respond to rising air current (thermals) in order to extend endurance and gain altitude with minimal use of the motor (soaring). Its full technical description is available in
S. Tabor, I. Guilliard, A. Kolobov. ArduSoar: an Open-Source Thermalling Controller for Resource-Constrained Autopilots. International Conference on Intelligent Robots and Systems (IROS), 2018.
Use of an airspeed sensor is strongly recommended in order to obtain optimum performance. Use without a sensor could yield unsatisfactory results. Consistent operation without an airspeed sensor is a pending future development.
This picture shows the different phases of flight when using the soaring functionality:
If modes AUTO, FBWB or CRUISE are entered, and Soaring is enabled, the throttle is set to zero provided the aircraft is above SOAR_ALT_MIN altitude and the aircraft then begins gliding.
In AUTO, if the aircraft descends to SOAR_ALT_MIN altitude, throttle is re-enabled and the aircraft will begin to climb to the altitude of the next waypoint. If that waypoint altitude is less than SOAR_ALT_CUTOFF altitude, then Soaring can not begin before reaching the waypoint. If it is above SOAR_ALT_CUTOFF altitude, then Soaring can occur once that altitude has been reached. In FBWB or CRUISE modes, if SOAR_ALT_MIN altitude is reached, an RTL will be initiated, so the pilot must disable Soaring, or change to a mode other than FBWB or CRUISE to climb back above SOAR_ALT_CUTOFF to begin gliding again and prevent an RTL beginning.
When the aircraft reaches SOAR_ALT_CUTOFF altitude, throttle is set to zero again.
If, during gliding flight, the air is estimated to be rising at more than SOAR_VSPEED and the RC switch position allows it, the aircraft will automatically enter LOITER mode. While in LOITER mode the aircraft will adjust the loiter position to better centre the thermal.
LOITER mode is exited under the following conditions:
SOAR_ALT_MAX is reached.
SOAR_ALT_MIN is reached.
Flight mode is changed by the pilot.
The flight mode will be returned to whatever it was before LOITER was triggered. As an exception to this, if the previous mode was FBWB or CRUISE, and thermalling ended due to reaching SOAR_ALT_MIN, RTL will be triggered instead.
To use your plane for soaring, it should ideally be a glider type aircraft with a good lift to drag ratio and be equipped with an airspeed sensor.
Generally all boards support soaring, except those with firmware limitations referred to on this page. As of June 2020, non-supported boards include:
Set TECS_SPDWEIGHT to 2.0. This makes sure the aircraft will glide correctly with motor off.
Set the parameter SOAR_ENABLE to 1 and refresh the parameters. This will allow the other SOAR parameters to appear in the GCS.
To work out how fast the air is rising or sinking the autopilot needs to know the aircraft’s sink rate for a given airspeed in still air. This is related to the drag polar of the plane and is specified using the SOAR_POLAR parameters. SOAR_POLAR_K is the most important one to set initially and is calculated using the following formula:
SOAR_POLAR_K = 16*Weight/Area (weight in kg, area in metres squared).
SOAR_POLAR_K = 703*Weight/Area (weight in oz, area in inches squared).
Calculating the other parameters is explained under tuning.
RC switch (Optional)¶
You can use a 2-position RC switch to control when the autopilot can use soaring. Set the parameter SOAR_ENABLE_CH to the corresponding channel number. The 2 positions have the following effect.
Below 1700us. Soaring is disabled (equivalent to setting SOAR_ENABLE = 0). Throttle will be used as normal. Switching to this from either of the positions below, will disable Soaring and maintain the current flight mode.
Above 1700us. Fully automatic mode changes to LOITER from AUTO, FBWB or CRUISE modes in response to detected rising air, and following of rising air currents.
The parameter WP_LOITER_RAD sets how tight the loiter circle is. For thermalling it is usually best to have the aircraft fly at a 30 - 45 degree bank angle. The corresponding loiter radius can be calculated as about airspeed squared over ~10 (for 45 degrees) or ~6 (for 30 degrees), from the equation
The tangent is for the desired bank angle. The resulting radius will be in meters. Use g = 9.81 m/s/s, and velocity (v) is in m/s. For example, if the airspeed in loiter is 20m/s, then the WP_LOITER_RAD should be 40m for a 45 degree bank.
You should make sure that the limiting bank angle LIM_ROLL_CD is set a bit larger than the desired bank angle to give some room for manoeuvring.
Because the soaring feature can follow rising air as required to gain altitude, it is important to set limits to avoid it leaving the original flight area completely. This is especially important in windy conditions as the autopilot will try to follow thermals downwind.
Geofence can be used to constrain the physical flight area used. Set it up in the usual way.
SOAR_VSPEED controls when the mode will be changed to LOITER to begin thermalling. The default of 0.7m/s may be too low if you fly in strong conditions. Increasing this value makes the aircraft more “picky” about the lift it will try to circle in.
While the default settings for SOAR_POLAR_B and SOAR_POLAR_CD0 should be OK for most foamie-style glider aircraft, improving the accuracy of these parameters will improve how your aircraft detects and centres lift. You can use this spreadsheet to calculate better values from glide tests.
Adding hysteresis can reduce the frequency of mode changes.
SOAR_MIN_THML_S: Minimum time to remain in LOITER once entered for a thermal before exiting due to low lift or altitude limits.
SOAR_MIN_CRSE_S: Minimum time to remain in glide after exiting LOITER due to low lift or altitude limits before entering LOITER mode again, or when entering Soaring initially.
For best results the TECS needs to be set up to fly the aircraft at a consistent airspeed when gliding.
If your aircraft has trouble maintaining airspeed accurately you can tune it by confirming that TECS_SPDWEIGHT is set to 2.0, SOAR_ENABLE to 1 and set SOAR_VSPEED to a large number, say 50.0, or use the RC switch to inhibit mode changes. This means that the aircraft will glide but will never begin thermalling. Set SOAR_ALT_CUTOFF to an altitude high enough to allow a good length of time to be spent gliding.
Launch the aircraft and put it in AUTO mode. It should climb to SOAR_ALT_CUTOFF
and then begin a gliding descent. Watch the telemetry graphs or look at the Dataflash logs after the flight. Is the aircraft maintaining the demanded airspeed? The actual and demanded airspeed can be seen in the onboard log as
TECS.spdem, and via telemetry you can use
NAV_CONTROLLER_OUTPUT.aspd_error. Problems can usually be fixed
PTCH2SRV_IMAX and TECS_INTEG_GAIN to achieve good airspeed
tracking in gliding flight.
Use of TECS synthetic airspeed¶
If your plane can’t accommodate an airspeed sensor, it is possible to use the TECS synthetic airspeed estimate TECS_SYNAIRSPEED. Make sure you read the warning regarding this feature before deciding to use it. To use this feature, set the parameter TECS_SYNAIRSPEED to 1.