Title :
Analysis and design of BTT Autopilot with stable yaw rate
Author :
Lei, Wang ; Jing-yu, Di ; Tao, Guo
Author_Institution :
Flying Vehicle Eng. Dept., Beijing Inst. of Technol., Beijing, China
Abstract :
A design and analysis method of BTT Autopilot based on yaw rate stability is proposed. Based on the decoupled model of missile body, three-channels autopilot for a simplified missile model using classical control theory is independently designed, then carry out the 6DOF simulation of system. The results show that the method is appropriate for the coordinated turn control of BTT missile with slow turning rate, and the designed autopilot can follow the instructions quickly, and has a certain ability to resist interference.
Keywords :
missile control; stability; vehicle dynamics; 6DOF simulation; BTT; classical control theory; coordinated turn control; decoupled model; missile model; three-channels autopilot; yaw rate stability; Analytical models; Control systems; Damping; Missiles; Stability analysis; Systematics; Transfer functions; autopilot; bank-to-turn; cruise missile; yaw rate stability;
Conference_Titel :
Computer Science and Automation Engineering (CSAE), 2011 IEEE International Conference on
Conference_Location :
Shanghai
Print_ISBN :
978-1-4244-8727-1
DOI :
10.1109/CSAE.2011.5953321
