Hardware-in-the-Loop Simulation of an Extended Non-Linear Dynamic Inversion Augmented with an Immunity-Based Adaptive Control System

2013 ◽  
Author(s):  
Brendon Lyons ◽  
Hever Moncayo ◽  
Alfonso Noriega ◽  
Israel Moguel ◽  
Mario G. Perhinschi
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Dynamic Inversion ◽  
Hardware In The Loop ◽  
Adaptive Control System ◽  
Linear Dynamic ◽  
Non Linear

Design of Non-Linear Dynamic Inversion UAV with QFT

2012 ◽  
Vol 466-467 ◽  
pp. 676-679 ◽  
Author(s):  
Jie Li ◽  
Jie Zhang ◽  
Zhi Hui Xu
Keyword(s):  
Control System ◽  
Flight Control ◽  
Inversion Method ◽  
Dynamic Inversion ◽  
Model Errors ◽  
Flight Control System ◽  
Linear Dynamic ◽  
Performance Requirements ◽  
Non Linear ◽  
Aerial Vehicle

Flight control system of UAV (Unmanned Aerial Vehicle) has limitations with non-linear dynamic inversion method. This paper introduces QFT based on non-linear dynamic inversion method, for avoiding model errors during existing non-linear function offset, QFT theory is presented firstly, then UAV model is established using non-linear dynamic inversion method, definituding the range of errors and system performance requirements, flight control system of UAV is designed with QFT, the simulating curves show that system has robustness stability.

ADAPTIVE CONTROL SYSTEM FOR AIRCRAFT LONGITUDINAL MOTION

2012 ◽  
Vol 43 (5) ◽  
pp. 683-695 ◽  
Author(s):  
Yury Grigoryevich Zhivov ◽  
Alexander Mikhaylovich Poedinok
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Longitudinal Motion ◽  
Adaptive Control System

Model-reference adaptive control system

AIChE Journal ◽  
1967 ◽  
Vol 13 (3) ◽  
pp. 485-491 ◽  
Author(s):  
Robert M. Casciano ◽  
H. Kenneth Staffin
Keyword(s):  
Adaptive Control ◽  
Control System ◽  
Model Reference Adaptive Control ◽  
Adaptive Control System ◽  
Model Reference ◽  
Model Reference Adaptive
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