劣駆動小型自律航空機の非線形制御による着陸誘導(J16-1,J16 工学的応用に向けた複雑系の能動制御)

概要

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This paper presents a numerical simulation for longitudinal guidance of an autonomous aircraft using only a rudder. If an aircraft is miniaturized, a navigation system and control surfaces have potential to be insufficient. In this case, a controllability of aircraft decreases. Therefore, a stability of aircraft should be improved. And an aircraft is known as nonlinear, nonholonomic and under actuated system. Generally this kind of system is more difficult to be controlled compared to systems which have full set of control surfaces. This study proposes a guidance method which solves inverse problems by input-output relation to decide patternized input and shows numerically this method is effective for guidance of an aircraft.
社団法人日本機械学会の論文
2004-09-04