Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods. A representative unmanned aerial vehicle (UAV) comprises an airframe, a plurality of rotors, and a capture line. The rotors are coupled to the airframe and configured to support the UAV in hover. The capture line is carried by the UAV and is operatively coupled to an immersible anchor. The immersible anchor is configured to be immersed within a body of water during a capture operation involving the capture line.
AERIAL LAUNCH AND/OR RECOVERY FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS
2021-12-02
Patent
Elektronische Ressource
Englisch
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