AIR VEHICLE AND METHOD OF CONTROLLING AIR VEHICLE

A fuselage, a support part supporting the fuselage, a thrust generation unit including fore, aft, left, and right thrust generators, and a flight controller controlling the unit are included. The fore, aft, left, and right thrust generators are respectively positioned on first, second, third, and fo...

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Bibliographische Detailangaben
Hauptverfasser: KOUCHI, Kaoru, KATAYAMA, Noriaki
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A fuselage, a support part supporting the fuselage, a thrust generation unit including fore, aft, left, and right thrust generators, and a flight controller controlling the unit are included. The fore, aft, left, and right thrust generators are respectively positioned on first, second, third, and fourth axes respectively extending in support part fore and aft, fore and aft, left and right, and left and right directions. The generators are respectively at the support part front, back, left, and right. The generators respectively generate thrust in directions intersecting the first, second, third, and fourth axes and can change thrust magnitude and direction around them. All generators are connected to the support part.