DocumentCode
2799925
Title
Pole assignment method with state constraints for missile three-loop autopilot design
Author
Chao Chang ; De-fu Lin ; Jiang Wang
Author_Institution
Sch. of Aerosp. Sci. & Eng., Beijing Inst. of Technol., Beijing, China
fYear
2009
fDate
17-19 June 2009
Firstpage
3298
Lastpage
3301
Abstract
The three-loop autopilot is transformed into states space model, and the feasibility of presupposition of some nuisance parameter is proved. A new pole assignment method is studied. Considering the actuator state feedback constraints, search methods are used to find the additional poles introduced by actuator. The design results show that, with the new method, all the poles of the system can be assigned to the desired place.
Keywords
control system synthesis; missile guidance; pole assignment; state feedback; state-space methods; actuator state feedback constraint; missile three-loop autopilot design; nuisance parameter; pole assignment method; search method; state space model; Acceleration; Accelerometers; Actuators; Aerodynamics; Chaos; Feedback loop; Missiles; Robust stability; State feedback; State-space methods; pole assignment; state feedback constraints; three-loop autopilot;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference, 2009. CCDC '09. Chinese
Conference_Location
Guilin
Print_ISBN
978-1-4244-2722-2
Electronic_ISBN
978-1-4244-2723-9
Type
conf
DOI
10.1109/CCDC.2009.5192835
Filename
5192835
Link To Document