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。
The inverse dynamics model of superheated steam temperature is complex, nonlinear, whose solution is get more difficult by general method.
过热汽温对象的逆动力学模型是复杂的非线性模型，利用常规的求解方法很难求解。
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