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本文研究了空间飞行器自动对接控制系统的多变量频域逆奈氏阵列设计方法。首先建立了跟踪飞行器和目标飞行器相对运动的数学模型。然后根据最后接近阶段的飞行特点,给出了实现对角优势的新方法。最后将此方法应用于本文的实例中。
In this paper, we study the multivariable frequency-domain inverse Jena array design method of the spacecraft automatic docking control system. First of all, a mathematical model to track the relative movement of the aircraft and the target aircraft is established. Then based on the flight characteristics of the last approaching phase, a new method to realize the diagonal advantage is given. Finally, this method is applied to the examples in this article.