DocumentCode
2290855
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
Volume
1
fYear
2011
fDate
10-12 June 2011
Firstpage
734
Lastpage
737
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Science and Automation Engineering (CSAE), 2011 IEEE International Conference on
Conference_Location
Shanghai
Print_ISBN
978-1-4244-8727-1
Type
conf
DOI
10.1109/CSAE.2011.5953321
Filename
5953321
Link To Document