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鲁棒变结构制导规律研究
引用本文:侯明善.鲁棒变结构制导规律研究[J].上海航天,2000,17(4):40-43.
作者姓名:侯明善
作者单位:西北工业大学,陕西,西安,710072
摘    要:研究存在相对速度测量噪声时的鲁棒制导问题,根据一类变结构制导规律,分析了相对速度测量噪声、制导参数对导引收敛性的影响,以弹道收敛为准则,给出了实现鲁棒制导的条件,研究结果对设计先进的雷达制导系统具有重要意义。

关 键 词:测量噪声  鲁棒性  弹道收敛  制导规律

STUDY ON ROBUST VARIABLE STRUCTURE GUIDANCE LAW
HOU Ming-shan.STUDY ON ROBUST VARIABLE STRUCTURE GUIDANCE LAW[J].Aerospace Shanghai,2000,17(4):40-43.
Authors:HOU Ming-shan
Abstract:Measurement noise of sensor in guidance system is the main cause of degradation of guidance performance. To reduce its effects, a certain measure must be taken according to the signal to noise ratio in the guidance loop. In this paper, the robust guidance under the measurement noise of relative range rate is studied. A variable structure guidance law is first proposed, then two different cases are considered.The deterministic relationships that the guidance law parameters must meet for robust guidance and successful interception are presented. The results are very helpful to the designs of modern advanced radar guidance systems.
Keywords:Measurement noise  Robust guidance  Ballistic convergence
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