Title :
Design of autopilot with Pole placement and State-Observer Feedback
Author :
Lei, Wang ; Xiu-yun, Meng ; Qun-li, Xia ; Guo Tao
Author_Institution :
Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
Abstract :
A autopilot designing method with Pole placement Method and State-Observer Feedback is proposed. State feedback gain via pole placement is designed by selecting a suitable root of closed-loop transfer function. With poles placement method full-order state observer with one or two measurable outputs are designed respectively. By comparing time-domain outputs of the two observers, It is concluded that, observer with two measurable outputs can be more accurate in the observation on the original system state under the condition of guaranteeing Filter characteristics.
Keywords :
closed loop systems; missile guidance; observers; state feedback; transfer functions; autopilot design; closed-loop transfer function; missile; pole placement method; state feedback gain; state-observer feedback; Damping; Equations; Extraterrestrial measurements; Mathematical model; Observers; State feedback; Time domain analysis; autopilot; pole placement; state-observer; statefeedback;
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.2011.5952802