To provide a system which can more properly control flow of air around an airframe of an aircraft.SOLUTION: A control system 1 of an aircraft includes: a flow control device 16 controlling flow of air around an aircraft; and a control circuit controlling the flow control device 16 in such a way that a pressure distribution applied to a surface of a structure constituting the aircraft becomes a control value of the pressure distribution, which is calculated on the basis of a physical value related to the air around the aircraft and detected by a sensor 8 provided in the aircraft.SELECTED DRAWING: Figure 1
【課題】航空機の機体周りの空気の流れを、より適切に制御できるシステムを提供する。【解決手段】航空機の制御システム1は、航空機の周囲における空気の流れを制御する流れ制御デバイス6と、前記航空機を構成する構造体の表面に負荷される圧力分布が、前記航空機に備えられるセンサ8で検出される物理量であって前記空気に関連する前記物理量に基づいて計算される圧力分布の制御値となるように前記流れ制御デバイス16を制御する制御回路とを有する。【選択図】図1
AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD AND AIRCRAFT
航空機の制御システム、航空機の制御方法及び航空機
2019-06-06
Patent
Elektronische Ressource
Japanisch
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