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Sunlight-powered sustained flight of an ultralight micro aerial vehicle

Author

Listed:
  • Wei Shen

    (Beihang University)

  • Jinzhe Peng

    (Beihang University)

  • Rui Ma

    (Beihang University)

  • Jiaqing Wu

    (Beihang University)

  • Jingyi Li

    (Beihang University)

  • Zhiwei Liu

    (Beihang University
    Collaborative Innovation Center of Advanced Aero-Engine
    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics
    Beijing Key Laboratory of Aero-Engine Structure and Strength)

  • Jiaming Leng

    (Collaborative Innovation Center of Advanced Aero-Engine)

  • Xiaojun Yan

    (Beihang University
    Collaborative Innovation Center of Advanced Aero-Engine
    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics
    Beijing Key Laboratory of Aero-Engine Structure and Strength)

  • Mingjing Qi

    (Beihang University
    Collaborative Innovation Center of Advanced Aero-Engine
    National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics
    Beijing Key Laboratory of Aero-Engine Structure and Strength)

Abstract

Limited flight duration is a considerable obstacle to the widespread application of micro aerial vehicles (MAVs)1–3, especially for ultralightweight MAVs weighing less than 10 g, which, in general, have a flight endurance of no more than 10 min (refs. 1,4). Sunlight power5–7 is a potential alternative to improve the endurance of ultralight MAVs, but owing to the restricted payload capacity of the vehicle and low lift-to-power efficiency of traditional propulsion systems, previous studies have not achieved untethered sustained flight of MAVs fully powered by natural sunlight8,9. Here, to address these challenges, we introduce the CoulombFly, an electrostatic flyer consisting of an electrostatic-driven propulsion system with a high lift-to-power efficiency of 30.7 g W−1 and an ultralight kilovolt power system with a low power consumption of 0.568 W, to realize solar-powered sustained flight of an MAV under natural sunlight conditions (920 W m−2). The vehicle’s total mass is only 4.21 g, within 1/600 of the existing lightest sunlight-powered aerial vehicle6.

Suggested Citation

  • Wei Shen & Jinzhe Peng & Rui Ma & Jiaqing Wu & Jingyi Li & Zhiwei Liu & Jiaming Leng & Xiaojun Yan & Mingjing Qi, 2024. "Sunlight-powered sustained flight of an ultralight micro aerial vehicle," Nature, Nature, vol. 631(8021), pages 537-543, July.
  • Handle: RePEc:nat:nature:v:631:y:2024:i:8021:d:10.1038_s41586-024-07609-4
    DOI: 10.1038/s41586-024-07609-4
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