The pilot's optimal control 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 flight control law is designed by using nonlinear inverse dynamics and modern optimal control theory.

针对12维非线性飞机动力学模型，利用非线性逆系统理论和现代最优控制理论设计了一组非线性飞行控制规律。

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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.

提出了现代飞行控制系统的优化设计需考虑驾驶员的操纵行为和生理限制，才能进行人-机组合优化设计。

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