Simulation Analysis of Tracking and Control Link Level in Launch Vehicle Based on STK

Qian He, G. Wu
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引用次数: 0

Abstract

The target feature analysis is essential for sea based launch vehicle tracking and control. The analysis method is performed with recognizing gain changes of telemetry antenna pattern in task usually and computing the automatic gain control (AGC) signal received by TT &C station manually. Aiming at the problems of low efficiency, complicated process and human errors, the method is discussed for a simulation analysis of tracking and control link level in launch vehicle based on STK, which elaborated emphatically for generating the electromagnetic field radiation pattern accord with STK format by launch vehicle antenna pattern. Compare the results of simulation and actual tracking by the launch vehicle in a flying, it indicates that the proposed method can satisfy the requirement in task and the result of simulation can be the reference by target feature analysis on launch vehicle.
基于STK的运载火箭跟踪控制链路水平仿真分析
目标特征分析是海基运载火箭跟踪与控制的关键。分析方法通常是在任务中识别遥测天线方向图的增益变化,并人工计算测控站接收到的自动增益控制(AGC)信号。针对效率低、过程复杂和人为误差等问题,讨论了基于STK的运载火箭跟踪与控制链路水平仿真分析方法,重点阐述了利用运载火箭天线方向图生成符合STK格式的电磁场辐射方向图的方法。仿真结果与实际运载火箭飞行跟踪结果的对比表明,所提出的方法能够满足任务要求,仿真结果可为运载火箭目标特征分析提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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