现代防御技术2011，Vol.39Issue(4)：19-25,7.DOI:10.3969/j.issn.1009-086x.2011.04.005
一种旋转导弹解耦控制方法
One Method of Decoupling for Spinning Missiles
杨立峰 1闫晓勇2
作者信息
- 1. 海军驻北京舰空导弹系统军事代表室,北京100854
- 2. 北京电子工程总体研究所,北京 100854
- 折叠
摘要
Abstract
The control method based on frequency coupling degree of stability theory was studied for coupling of spinning missiles. The dynamic stability' s judgment was brought by Nyquist array technique, and the coupling degree of spinning missiles for different rolling speed was analyzed in allusion to practical illustration, then, the effect of servo and body dynamics for coupling resonance frequency was obtained. Based on the requirement of develop project, the method of decoupling controller design was e-duced and was validated.关键词
旋转导弹/解耦控制/多变量Key words
spinning missile/ decoupling control/ multivariable分类
军事科技引用本文复制引用
杨立峰,闫晓勇..一种旋转导弹解耦控制方法[J].现代防御技术,2011,39(4):19-25,7.
