The Rolling Angle Feedback Based Coordinated Stable Control Law Design of UAV
The coordinated stable control of an UAV with the R&A task is considered in this paper. Arc circle is introduced before turning to reduce recognition difficult of electro-optical pod. The integrated guidance and control system design method is used for UAV due to the good characters of the pitching mode, rolling mode and Dutch Roll mode of the linearized ontology mode. The altitude hold strategy and rolling angle feedback based coordinated turning strategy are applied respectively to accomplish the reconnaissance and attack (R&A) task. The six freedom degree simulations are given to illustrate the efficiency of the proposed method.
aircraft control unmanned aerial vehicle (UA V) coordinated stability integrated guidance and control (IGC)
Ying Jing Shi Rui Li
Institute of Astronautics and Aeronautics University of Electronic Science and Technology of China C School of Automation University of Electronic Science and Technology of China Chengdu, China
国际会议
重庆
英文
553-557
2011-01-21（万方平台首次上网日期，不代表论文的发表时间）