Simulation and analysis of one missile control system based on guidance control theory and method

被引：0
|
作者：
Ouyang, X [1 ]
Wang, GL [1 ]
Li, J [1 ]
Yang, J [1 ]
Zhang, YS [1 ]
机构：
[1] Mech Engn Coll, Shijiazhuang 050003, Hebei, Peoples R China
来源：
ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings | 2005年
关键词：
simulation; control system; guidance law;
D O I：
暂无
中图分类号：
TH7 [仪器、仪表];
学科分类号：
0804 ; 080401 ; 081102 ;
摘要：
In this paper a novel guidance control theory and method based on one missile control system is proposed. By regarding target maneuvers as disturbances parameters input, we reformulate that the missile guidance problem is one kind of disturbance attenuation control problem. It is important for missile design and system simulation and test. By theory analysis and system simulation the results showed that the new guidance law has strong robustness and excellent interception results against the maneuvering targets. And it is used in one missile control system design and simulation.
引用
收藏
页码：7796 / 7799
页数：4
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