DocumentCode
3862744
Title
Research on algorithm of nonlinear self-adaptive flight control system
Author
Hao Long;Sujie Song
Author_Institution
College of Automation, Beijing Union University, Beijing 100101, China
fYear
2015
Firstpage
332
Lastpage
336
Abstract
For the nonlinear control problem of Super-maneuver aircraft, a nonlinear flight control law was presented base on the nonlinear structure adaptive model inversion system,. The sufficient and necessary condition of the control law was analyzed. Finally the results of the height-angle maneuver simulation shows that the designed control system has good performance.
Keywords
"Decision support systems","Mechatronics","Adaptive systems","Adaptation models","Aerospace control","Manganese"
Publisher
ieee
Conference_Titel
Advanced Mechatronic Systems (ICAMechS), 2015 International Conference on
Electronic_ISBN
2325-0690
Type
conf
DOI
10.1109/ICAMechS.2015.7287084
Filename
7287084
Link To Document