CREWLESS AIRCRAFT, SYSTEM, AND CONTROL METHOD

An unmanned aerial vehicle (10m) includes: a vehicle main body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; propellers (22) that rotate in a virtual plane parallel to the first and second directions;...

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Bibliographische Detailangaben
Hauptverfasser: KATO, Tatsuya, TAKAHAMA, Takuya, AOYAMA, Hideki, AMAGAI, Ryosuke, SASAKI, Gaku, OSHIMA, Mitsuaki, HAYASHI, Nobuaki, TANIUCHI, Naoyuki, MURAMATSU, Fumio, KITAZAWA, Kazuma
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:An unmanned aerial vehicle (10m) includes: a vehicle main body (1912) having a first length (N1) in a first direction longer than a second length (N2) in a second direction orthogonal to the first direction; propellers (22) that rotate in a virtual plane parallel to the first and second directions; first propeller actuation motors (23) that are provided on the vehicle main body (1912) and respectively rotate the propellers (22); at least one connector (1720) that is hangable from at least one rail (7) spaced apart from the ground surface; at least one side propeller (22a1) that provides propulsion force for propelling the vehicle main body (1912) in the first direction; at least one third propeller actuation motor (22a3) that is provided on the vehicle main body (1912) and rotates the at least one side propeller (22a1); and a control processor (11) that controls the first propeller actuation motors (23) and the at least one third propeller actuation motor (22a3).