到達限界を用いた航空機の編隊変更の最短時間導出法

抄録

In this paper, a method to derive the minimum-time for formation reconfiguration of cruising two fixed-wing aircraft is proposed. Conventionally, the optimal reconfiguration problem is formulated as an optimal control problem by treating the aircraft as one system. In this paper, it is shown that the solution for this problem is driven by solutions for optimal control problem of single aircraft. The terminal values of this problem, which mean reachable limits of each aircraft, are consolidated efficiently, providing the time for the reconfiguration.