Adaptive Model Inversion Flight Control for Tilt-Rotor Aircraft

1999 ◽  
Vol 22 (3) ◽  
pp. 402-407 ◽  
Author(s):  
Rolf T. Rysdyk ◽  
Anthony J. Calise
Keyword(s):  
Flight Control ◽  
Adaptive Model ◽  
Model Inversion ◽  
Tilt Rotor

Design of the Nonlinear Structure Adaptive Model Inversion Flight Control System

2016 ◽  
Vol 28 (6) ◽  
pp. 928-935
Author(s):  
Hao Long ◽  
◽  
Yi-Nung Chung ◽  
Keyword(s):  
Control System ◽  
Nonlinear Control ◽  
Flight Control ◽  
Necessary Condition ◽  
Adaptive Model ◽  
Flight Control System ◽  
Nonlinear Structure ◽  
Model Inversion ◽  
Text Design ◽  
Sufficient And Necessary Condition

[abstFig src='/00280006/17.jpg' width='300' text='Design of the nonlinear SAMI flight control system' ] The advanced aircraft has those technological characteristics: stealth, supersonic cruise, super maneuverability, multi-target attack, multi-role, high load, long range cruise, integrated avionics, short takeoffs and vertical landings. These characteristics need multi-subsystem integration in the advanced aircraft. In order to meet the need of advance aircraft, the nonlinear control system is necessary. In this paper, the nonlinear structure adaptive model inversion system was first used for the nonlinear control problem of super-maneuver aircraft. The sufficient and necessary condition of the control law was analyzed. Finally the results of the height-angle maneuver simulation show that the designed control system has good performance.

Adaptive model inversion flight control for tiltrotor aircraft

1997 ◽  
Author(s):  
Anthony Calise ◽  
Rolf Rysdyk ◽  
Anthony Calise ◽  
Rolf Rysdyk
Keyword(s):  
Flight Control ◽  
Adaptive Model ◽  
Model Inversion ◽  
Tiltrotor Aircraft

Adaptive Model Following Systems for Flight Control and Simulation

1972 ◽  
Vol 9 (9) ◽  
pp. 668-674 ◽  
Author(s):  
I. D. LANDAU ◽  
B. COURTIOL
Keyword(s):  
Flight Control ◽  
Adaptive Model ◽  
Model Following

Novel Control Scheme for Helicopter Flight: Fuzzy Immune Adaptive Model Inversion Control

2008 ◽  
Vol 41 (2) ◽  
pp. 15046-15051 ◽  
Author(s):  
Zhao Jia ◽  
Chen Shenggong ◽  
Shen Gongzhang
Keyword(s):  
Adaptive Model ◽  
Model Inversion ◽  
Helicopter Flight ◽  
Control Scheme
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