DocumentCode :
2843184
Title :
Integrated guidance and control for a missile in the pitch plane based upon subspace stabilization
Author :
Baohua, Sang ; Changsheng, Jiang
Author_Institution :
Coll. of Aviation Technol., NUAA, Nanjing, China
fYear :
2009
fDate :
17-19 June 2009
Firstpage :
5409
Lastpage :
5414
Abstract :
Based upon the model of the relative motion between the missile and the target and the model of the missile moving in the pitch plane, a novel integrated guidance and control model under the error tracking meaning is established. It is different from the state equation based integrated guidance and control models, it emphasizes particularly on attitude angles tracking. Especially, the realization of the error tracking properties is turned into the corresponding parameters adjusting by subspace stabilization technology. The globally asymptotical stabilization of the error tracking system is realized by an observer with the adaptive adjusting function about the model error and about the target maneuverability. The simulation results indicate that the design is effective.
Keywords :
adaptive control; asymptotic stability; missile control; missile guidance; observers; position control; target tracking; adaptive adjusting function; adaptive observer; asymptotic stabilization; attitude angles tracking; error tracking model; missile and target relative motion; missile control; missile guidance; pitch plane; subspace stabilization; subspace stabilization technology; target maneuverability; Adaptive control; Automatic control; Error correction; Missiles; Motion control; Navigation; Nonlinear equations; Programmable control; Sliding mode control; Target tracking; integrated guidance and control; missile; observer; subspace stabilization;
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.2009.5195157
Filename :
5195157
Link To Document :
بازگشت