Research on the fast nose-point control of a Fighter
The fast nose-point control of a fighter is researched in the frame of Integrated Control System with a multi-strata hierarchical structure. Based on the relationship between nose pointing rate and attitude angle, the nose pointing command including the normal load command and bank angle command is got to make the nose fast point to the expected direction by introducing the expecting nose pointing model. The actuator-allocation controller is designed as the maneuvering command tracker to execute the given command. Then, the nose pointing control is applied to the air to air gunnery mode of Integrated Flight/Fire Control in which the fast nose pointing control is the most important. The simulation result shows that the control methodology of nose pointing can fast eliminate the error of aiming.
LIAO Kai-jun DONG Xin-min WANG Xiao-ping CHEN Ya-li
The Engineering Institute,Air Force Engineering University,Xian 710038,China
国际会议
2009 IEEE International Conference on Information and Automation(2009年 IEEE信息与自动化国际学术会议)
珠海、澳门
英文
248-253
2009-06-22（万方平台首次上网日期，不代表论文的发表时间）