Control surface inverse algorithm and application to nonlinear H missile control

Chien Chung Kung, Ciann Dong Yang, Keng Lon Lei

研究成果: Conference contribution

1 引文 斯高帕斯(Scopus)

摘要

The proposed nonlinear H_inf missile autopilot in this paper is to resist maximal possible disturbances and counterbalance vortex-induced yawing moments during high AOA flight. The implementation of the nonlinear H_inf missile autopilot is solved by the control surface inverse algorithm (CSIA). The CSIA is an algorithm to compute the associated control surface deflections based on minimizing the global errors between the commands and actual control forces and moments. The derivations of the control law, the control surface inverse algorithm of the autopilot and the satisfying results of the heading reversal maneuver are demonstrated in this paper.

原文English
主出版物標題Proceedings of the IEEE Conference on Decision and Control
發行者Institute of Electrical and Electronics Engineers Inc.
頁面5456-5461
頁數6
ISBN(列印)0780379241
DOIs
出版狀態Published - 2003
事件42nd IEEE Conference on Decision and Control - Maui, HI, United States
持續時間: 2003 12月 92003 12月 12

出版系列

名字Proceedings of the IEEE Conference on Decision and Control
5
ISSN(列印)0743-1546
ISSN(電子)2576-2370

Other

Other42nd IEEE Conference on Decision and Control
國家/地區United States
城市Maui, HI
期間03-12-0903-12-12

All Science Journal Classification (ASJC) codes

  • 控制與系統工程
  • 建模與模擬
  • 控制和優化

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