To provide an aircraft position control system and the like capable of stably sustaining a position of an aircraft in the air even when a target landing point fluctuates.SOLUTION: An aircraft position control system sustains an aircraft at a target coordinate point in the air with respect to a fluctuating target landing point, and includes: an acceleration correction processing unit that outputs a first posture correction acceleration for correcting an acceleration of the aircraft on the basis of the acceleration and a posture of the aircraft; a complementary filter that outputs a second posture correction acceleration which is obtained by removing a drift component contained in the first posture correction acceleration, on the basis of the first posture correction acceleration and an inertial velocity of the aircraft; and a smoothing processing unit that outputs smoothing relative coordinates which are obtained by smoothing relative coordinates, on the basis of the second posture correction acceleration and the relative coordinates between the aircraft and the target landing point.SELECTED DRAWING: Figure 4
【課題】目標着地点が動揺する場合であっても、空間上における航空機の位置を安定的に保持させることができる航空機の位置制御システム等を提供する。【解決手段】動揺する目標着地点に対して、空間上の目標座標に航空機を保持させる航空機の位置制御システムであって、航空機の加速度と航空機の姿勢とに基づいて、航空機の加速度を補正するための第1姿勢補正加速度を出力する加速度補正処理部と、第1姿勢補正加速度と航空機の慣性速度とに基づいて、第1姿勢補正加速度に含まれるドリフト成分を除去した第2姿勢補正加速度を出力する相補フィルタと、第2姿勢補正加速度と、航空機と目標着地点との間の相対座標とに基づいて、相対座標を平滑化した平滑化相対座標を出力する平滑化処理部と、を備える。【選択図】図4
AIRCRAFT POSITION CONTROL SYSTEM, AIRCRAFT, AND AIRCRAFT POSITION CONTROL METHOD
航空機の位置制御システム、航空機、及び航空機の位置制御方法
2022-05-25
Patent
Elektronische Ressource
Japanisch
AIRCRAFT POSITION CONTROL SYSTEM, AIRCRAFT, AND AIRCRAFT POSITION CONTROL METHOD
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