The pilot's optimalcontrol model is investigated. The optimal design destination function and method of flight controlling system have been proposed.
建立了驾驶员最优控制模型,提出了飞行控制系统优化设计目标函数和设计方法。
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Based on 12-state nonlinear aircraft dynamic model, a nonlinear flightcontrol law is designed by using nonlinear inverse dynamics and modern optimal control theory.
This paper proposes that it is necessary to concern the pilot's control behavior and human limits during the optimal design of modern flight controlling system.