DocumentCode
2344474
Title
Research on speediness stability of flight vehicle based on maximum principle
Author
Yao, Jun ; Wang, Xin ; Chen, Tao ; Wang, Yuxin
Author_Institution
Shenyang Ligong Univ., Shenyang
fYear
2008
fDate
3-5 June 2008
Firstpage
1200
Lastpage
1203
Abstract
Based on modern optimization control maximum principle, the results of optimization control moment are given on the condition that the range of aircraft roll disturbance is fixed and the control is restricted. This method can conquer the disturbance of roll in the shortest time, which can ensure the stability of flight.
Keywords
aerospace control; aircraft; optimisation; vehicle dynamics; velocity control; aircraft roll disturbance; flight stability; flight vehicle; optimization control maximum principle; optimization control moment; speediness stability; Aerospace control; Aircraft; Boundary conditions; Constraint optimization; Control theory; Differential equations; Mathematical model; Stability; TV broadcasting; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications, 2008. ICIEA 2008. 3rd IEEE Conference on
Conference_Location
Singapore
Print_ISBN
978-1-4244-1717-9
Electronic_ISBN
978-1-4244-1718-6
Type
conf
DOI
10.1109/ICIEA.2008.4582708
Filename
4582708
Link To Document