基于非线性动态逆理论，设计了亚轨道可重复使用运载器（SRLV）的再入控制律。

The objective of this paper is to design the reentry flight control laws for the Suborbital Reusable Launch Vehicle(SRLV) based on nonlinear dynamic-inversion.

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本文运用飞行力学原理和现代控制理论，对攻击地面固定目标的飞行器的再入机动制导方法进行了研究。

In this paper, the method of reentry maneuver guidance applying to attack the ground fixed target is described by using flight dynamics principle and modern control theory.

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适当地结合规划-跟踪算法和航迹角控制器可给再入制导带来极大的灵活性和适应性。

Proper combination of planning-tracking algorithm and FPA controller can bring great flexibility and adaptability to reentry guidance.

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