flight control law design 飞行控制律设计
reentry flight control law 再入控制律
The LQ is adapted to the flight control law design such as the Normal Acceleration control system.
并以法向过载控制模态为例，将线性二次型运用到飞行控制系统的控制律设计中。
Thus, an approach of Flight Control Law (FCL) model design and application for aircraft conceptual design is researched.
为此，本文进行了飞机总体设计中的飞行控制律模型设计与应用方法研究。
A robust nonlinear flight control law was proposed which synthesized the neural networks and the dynamic nonlinear damping theory.
应用神经网络控制与动态非线性阻尼控制综合的非线性控制方法对飞行控制律进行了研究。
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