摘要
针对先进气动布局飞机多操纵面的特点,将多操纵面控制分配问题转化为具有约束条件的最优化目标求值问题,将操纵指令合理地分配到各个操纵面上,最大程度满足飞机的操稳特性,解决了冗余的多操纵面控制分配问题。仿真结果确定了飞机在不同飞行任务下各个通道的操纵面控制分配方案。
In order to resolve the control allocation problem of the advanced aerodynamic configuration aircraft with multi-control-effectors,a method transforming the control allocation problem into constrained optimization evaluation problem is brought forward.Based on this method,the control inputs are allocated to each effector reasonably,insuring the controllability and stability of the aircraft,it can deal with redundant control effectors directly.The simulation results identify the scheme that can handle the tradeoff control allocation under various flight missions.
引文
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