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Observer-based Guidance Law Accounting for Second-order Dynamics of Missile Autopilots

Ping-Ping Qu Di Zhou

哈尔滨工业大学学报（英文版）2013，Vol.20Issue(1)：17-22,6.

Observer-based Guidance Law Accounting for Second-order Dynamics of Missile Autopilots

Ping-Ping Qu ¹Di Zhou²

作者信息

1. Dept.of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
2. School of Electronics and Information Engineering, Shenyang Aerospace University, Shenyang 110136, China
折叠

摘要

关键词

missile/guidance law/dynamic surface control/autopilot/observer

Key words

missile/guidance law/dynamic surface control/autopilot/observer

分类

航空航天

引用本文复制引用

Ping-Ping Qu,Di Zhou..Observer-based Guidance Law Accounting for Second-order Dynamics of Missile Autopilots[J].哈尔滨工业大学学报（英文版）,2013,20(1):17-22,6.

基金项目

Natural Science Foundation of China (Grant No.61174203),the Program for New Century Excellent Talents in University (Grant No.NCET-08-0153),and the Aviation Science Foundation of China(Grant No.20110177002). （Grant No.61174203）

哈尔滨工业大学学报（英文版）

ISSN：1005-9113

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