To provide a control method of a flight vehicle that can keep even an airframe having odd-number of propelling rotors in a horizontal attitude, and a flight vehicle.SOLUTION: In a control method of a flight vehicle UVA, which controls the fight vehicle UVA having an airframe B and odd-number of propelling rotors R, rotation speeds of the odd-number propelling rotors R and inclinations of rotating shafts of the odd-number of propelling rotors R with respect to the airframe B are adjusted so that component force in a horizontal direction, which generates torque FB that offsets torque FA for rotating the airframe B around a gravity center caused by reaction torque generated by the odd-number of propelling rotors, is generated, where the odd-number of propelling rotors R are provided so that inclinations of rotating shafts of the propelling rotors R with respect to the airframe B can be changed.SELECTED DRAWING: Figure 1
【課題】奇数個の推進ロータを有する機体であっても、機体を水平に維持することができる飛行体の制御方法および飛行体を提供する。【解決手段】飛行体UVAの制御方法は、機体Bと、奇数個の推進ロータRと、を有する飛行体UVAの制御方法であって、奇数個の推進ロータRは、推進ロータRの回転軸の機体Bに対する傾きが変更可能に設けられており、奇数個の推進ロータRが発生する反動トルクに起因する機体Bを重心回りに回転させるトルクFAを相殺するトルクFBを発生させる水平方向分力が発生するように、奇数個の推進ロータRの回転数および奇数個の推進ロータRの回転軸の機体Bに対する傾きを調整する。【選択図】図1
CONTROL METHOD OF ATTITUDE OF FLIGHT VEHICLE AND FLIGHT VEHICLE
飛行体の姿勢制御方法および飛行体
2023-03-17
Patent
Elektronische Ressource
Japanisch
IPC: | B64C AEROPLANES , Flugzeuge |
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