Hi everybody,

some of you might remember the 28-hour and 81-hour solar-powered flights (the world record in flight endurance for all aircrafts <50kg) by our Pixhawk-powered AtlantikSolar UAV that was presented here at diydrones last year. This year, we have not focused on records, but have been integrating more of our research at ETH Zurich. The result: The first-ever fully-autonomous (including launch, autonomous thermal updraft tracking and landing) solar-powered perpetual flight with significant payload (Color + Thermal Camera + Onboard Computer + WLAN for image live streaming) in a 26-hour Search-and-Rescue (SaR) mission.

From our website:

One year after having demonstrated the 81-hour continuous solar-powered flight that is still the current world record in flight endurance for all aircrafts < 50kg total mass, the AtlantikSolar UAV has completed its next milestone by demonstrating the first-ever fully-autonomous (from launch to landing) solar-powered perpetual flight with significant payload (Color + Thermal Camera) in a 26-hour Search-and-Rescue (SaR) mission. While the 81-hour and 28-hour endurance record flights were important milestones that demonstrated the perpetual endurance capability of AtlantikSolar, they required manual pilot control for launch and landing and did not carry any aerial imaging payload. However, the missions that our team really cares about – Search-and-Rescue missions relying on long-endurance aerial sensing to support authorities e.g. in the European refugee crisis currently unfolding over the Mediterranean Sea – require both of these elements, i.e. ease-of-use through full launch-to-land aircraft autonomy as well as significant payloads to help the rescue teams with the detection of victims on land and sea.

The 26-hour solar-powered Search-and-Rescue flight performed by AtlantikSolar AS-3 from July 19th – 20th 2016 demonstrated exactly that, and is therefore the first-ever flight world wide to combine:

  • Perpetual flight: 26-hours of solar-powered day/night- and thus energetically-perpetual flight
  • Full aircraft autonomy: No pilot stick moved within 26-hours of flight
  • SaR payload: The aircraft carried a 10 Watt 300g payload (1 Color camera, 1 Thermal Camera, 1 ODROID onboard computer with WLAN) and performed victim detection from the air during day and night.
  • Environment-aware: The aircraft performed automatic thermal updraft tracking for increased energetic efficiency and to speed up the battery recharge.

Flight summary

The 26-hour flight was started on July 19th at 18:02 local time in Hinwil, CH with full batteries. The launch was performed fully autonomously: After all system checks were complete, the aircraft was tossed in the air via a hand-launch and then continued automatically and without pilot interaction towards its first loitering waypoint. The respective flight control technology is based on an ETHZ/3DR Pixhawk autopilot with a custom flight controller designed at the Autonomous Systems Lab. Equipped with a color camera, thermal camera, an onboard computer and wireless LAN, the aircraft began live-streaming the respective images. The full payload was operated until around 21 o’clock, after which the color camera was switched off because of the insufficient lighting conditions. The batteries were at 95% state of charge at that time, having started their discharge shortly before 20 o’clock. Note that operating a fully fledged SaR payload consuming 10W is a significant challenge for perpetual flight on a small-scale solar-powered UAV such as AtlantikSolar, and the overall power consumption of ~60W was thus closely tracked during the first hours of the evening flight.

The actual testing of the Search-and-Rescue capabilities were started shortly before 23 o’clock: With the aircraft now flying in total darkness, the infrared camera served as the only source of aerial imaging information. As visible in the video, the payload system clearly manages to find the victim lying in low grass (and surrounding houses, tents, cars, the streets and especially the warm electric generator) at 23:05 o’clock. The victim detection was performed manually by the ground station operator based on the live-streamed images this time. However, the next AtlantikSolar test flight will have automatic on-board victim detection (as already tested in the ICARUS search and rescue project) implemented. The demonstrated capabilities are integral elements of perpetual flight aerial victim detection missions – we are convinced that they can be of great help in solving pressing issues such as the European refugee crisis of 2015 and 2016 above the Mediterranean Sea.

Despite heavy winds of up to 8m/s, the Search-and-Rescue support activities with the infrared camera payload were continued throughout the rest of the night. First sun was hit at 06:20 local time on July 20th, and the minimum battery state of charge was reached with 26% battery energy remaining at 08:04 o’clock. Considering the additional payload power consumption (and mass) of 10W , this energetic margin – achieved on July 20th, and thus about one month after the solar solstice on June 21st – is a success and even exceeds the margin of 23% predicted by our simulations. To accelerate the battery recharging process, the aircraft also implemented autonomous thermal updraft tracking that was enabled during the late morning once thermal updrafts were encountered (see video). Multiple “free” altitude gains of >100m were achieved this way – again without any pilot interaction. The batteries were fully re-charged at 15:30 o’clock.

As a final step, and after 26-hours of solar powered flight, the aircraft performed a fully autonomous landing at the Hinwil, CH airfield. Using its lightweight LIDAR (Light Detection And Ranging) sensor to measure its distance to the ground, AtlantikSolar – a hard to fly aircraft that can usually only be steered and landed by extremely experienced pilots – could safely perform the automatic landing. We consider the demonstrated full flight autonomy a vital step to allow search-and-rescue support teams, which usually do not possess extensive UAV flight training, to benefit from the signficant advantages of solar-powered and in general high-performance UAVs.

Further information

Detailed design and technical information on the UAV platform can be found in “Oettershagen P, Melzer A, Mantel T, Rudin K, Lotz R, Siebenmann D, Leutenegger S, Alexis K, Siegwart R (2015), A Solar-Powered Hand-Launchable UAV for Low-Altitude Multi-Day Continuous Flight. In: IEEE International Conference on Robotics and Automation (ICRA)” [Download] . An additional up-to-date publication including the research for this flight is planned.

Some more impressions from the flight were broadcasted live through our twitter account


This research was funded through the research project SolAIR – Solar-powered Automated Aerial Imaging and Reconnaissance Using Infrared Cameras. SolAIR is a project funded under Armasuisse contract #043-12. The AtlantikSolar project is in addition funded with ETH Zurich’s internal resources, private supporters, and the European Union FP7 Search-And-Rescue research projects ICARUS and SHERPA . Multiple project partners and collaborators have contributed towards making this important milestone possible, and we’d like to thank all of them for their various and ongoing support. Finally, we are grateful towards the Hinwil and Rafz model aeroplane clubs for providing the airfield!

Pilots: Rainer Lotz, Adrian Eggenberger. Development and Operations Team (Autonomous Systems Lab): Philipp Oettershagen, Rainer Lotz, Amir Melzer, Thomas Mantel, Bartosz Wawrzacz, Konrad Rudin, Thomas Stastny, Timo Hinzmann, Dieter Siebenmann, Dr. Gregory Hitz, Prof. Dr. Roland Siegwart.

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  • Hi Sam

    good to hear from you! I am just trying to push back some code to one of your repos - NOT to the ardupilot one (because as mentioned, we use the Pixhawk firmware) but to your simulation repository at https://github.com/samuelctabor/Soaring simulation that I extended quite a bit. I will create a pull request in ~3 weeks. You also have a private message / friend request about this, probably it is more efficient to discuss that way.



  • Hi Philipp,

    Nice project and glad that you found my soaring code useful. This has now been merged into the ardupilot master repo so now would be a good time to contribute your enhancements back to the codebase.



  • @Chris Jackson:

    Is this publication of any help? That publication is about the 28-hour flight last year, it should answer your motor questions and hint towards the optimal airspeed. The exact optimum power airspeed is of course a bit changed for this flight because we had 3.5kg instead of 2.9kg batteries in the plane and were carrying the ~300g payload. The power optimal point was thus ~60W (with the 10W payload) and 9.3m/s this time.


    See the initial publication. We did exactly this test there, i.e. no solar cells, only flying with batteries. We reached 12-15 hours. That should be a bit less considering that we had no payload (10W, 300g for this flight) in there, so you can assume 10-12 hours of flight time. Whether it is worth putting solar cells is then of course completely application-dependant.

    @Francisco Ferreira

    Of course you are right, the correct term is "PX4 firmware" (i.e. it is forked from https://github.com/px4/), but the term "Pixhawk firmware" is commonly used and probably better known in general. Ardupilot is used nowhere in our code. Also note that a) the thermal updraft tracking is just a tiny part in this project / video, b) Sam's way of handling the thermal updraft tracking is a commonly used one that is in similar form by many other authors, and c) the thermal updraft tracking was completely rewritten/changed and extended for Pixhawk. But of course the final scientific publication (and/or potential code-release to the Pixhawk firmware) will give suitable credit to all concepts and code (and their authors/developers) that this development is based on, no worries.

  • @Philipp Oettershagen

    You said your flight controller is based on the Pixhawk firmware, but, as far as I'm aware, no such thing exists. You either forked ArduPilot or PX4 and are running it in a Pixhawk board.

    From the comments you wrote, we now know that you based part of your work in Sam Tabor's fork of the ArduPilot Plane (ArduPlane) firmware. I found it odd that in all of your acknowledgements in the announcement and in your website I couldn't find Sam's name anywhere. ArduPilot also isn't mentioned, but that depends on exactly what code you based your work in. I believe this was just a neglect on your part and it will be corrected.

    As a fellow European, it is great to see EU money put up to good use. Thanks for sharing your progress with us.

  • MR60

    impressive. i wonder though how long you could fly on batteries alone without solar charging in the exact same setup, with less weight removing the solar panels and cabling, using the thermals as you did. in other words for how much of "net endurance" do the solar panels contribute really? I doubt of their real usefulness for the application since you could already fly many hours and long enough probably without them?

  • Very very impressive. Are you able to share any of your power system details? It sounds like a planetary box, and power draw is ~50W in a cruise, at what airspeed? 

  • @Jesus A

    Actually, the code managing the thermal updraft tracking is a port (and extension!) of this http://diydrones.com/profiles/blogs/ardusoar-cross-country-x-plane-... here to Pixhawk, and yes, our plan is to push that back to the main repo if there is interest from the developer side.

    @robert bouwens

    Also see the answer to Jesus A. Regarding the passive thermal compliance (i.e. the fact that the aircraft will just be "carried up with a thermal" instead of fighting it and trying to get down again), this is actually not a complicated implementation. See our publication. It's mostly just setting the speed weight parameter of TECS to 2.0 and avoiding that the integrator winds up during the time when h>h_ref. But currently there are now plans on our side to re-integrate that into the main pixhawk firmware because we have a completely different control infrastructure. If you are interested to re-integrate this for gliders, then we'd be happy to support your efforts of course.

    @Chris Cloutier

    As mentioned in our publication, this is the MPPT brain / chip, and there is even a reference design of this available here !

    @Global Innovator:

    Interesting approach, but you are aware of the effects of scaling on the aerodynamics (much lower efficiency once you operate below a certain Reynolds number) described in section 6.2 here ? Could you specificy again what you mean by "Is your team closed, project closed... ? " ?

  • @Philipp Oettershagen

    my congratulations on  your success.

    I am sure, Bertrand and Andre carefully watch your success story.

    Let me know if your Atlantik Solar can be scaled down to let me build much smaller version of your all-solar fixed-wing plane at Open Technology Lab.

    I have read your papers, technical specification, manual, I can laminate semi-flexible solar cells.

    My target is to make 4W single solar cell to fly.

    Since a single 4W solar cell has 0.5-0.6 voltage output I was trying to find 0.5 DC-DC step-up inverter and failed.

    3V DC-DC step-up inverter is available to power up electronics with 5V a more.

    I am looking for a lightweight fixed-wing plane and plan to install few solar cells as cargo to perform a number of live tests then upgrade it with a larger number of solar cells ( as cargo) to charge installed battery.

    So my approach is exactly the inverse.

    Let me know your opinion.

    Is your team closed, project closed for the development of mini all-solar fixed-wing planes ?

  • @phillip,

    i just like to build a glider. and it looks the tecs enhancement can catch thermals.

  • Fantastic work!  The continuous milestones this project keeps on achieving always amazes me. Would you be kind enough to share any detailed information about the MPPT?  Thank you.

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