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Methodology of Clearance of Flight Control Law

机译:飞行管制法清关的方法论

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摘要

This paper analysis the methodology of flight clearance and presents an example to verify the correctness and feasibility of the methods used in flight clearance process. The main goal of flight clearance is to try structured singular value (μ) analysis on the flight control system when some parameters in the system vary in a certain range. As μ- analysis can only be done on a linear fractional transformation (LFT) model, the first step of flight clearance is to generate the LFT model of the flight control system. An X-Fighter is chosen to realize the methods proposed in this paper. Simulation results demonstrate that X-Fighter passes the flight clearance. It not only proves the robustness of the control law but also confirms the correctness and feasibility of the methods used in the flight control process.
机译:本文分析了飞行清除的方法,并提出了一个例子,以验证飞行空间过程中使用的方法的正确性和可行性。飞行清除的主要目标是在系统中的某些参数在一定范围内变化时尝试在飞行控制系统上进行结构性奇异值(μ)分析。由于μ-分析只能在线性分数变换(LFT)模型,飞行间隙的第一步是产生飞行控制系统的LFT模型。选择X-Fighter以实现本文提出的方法。仿真结果表明,X战斗机通过了飞行清除。它不仅证明了对照法的稳健性,还证实了飞行控制过程中使用的方法的正确性和可行性。

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