Design of the Nonlinear Structure Adaptive Model Inversion Flight Control System | Zendy

Hao Long | Zendy; YiNung Chung | Zendy

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Design of the Nonlinear Structure Adaptive Model Inversion Flight Control System

Author(s) -

Hao Long,

YiNung Chung

Publication year - 2016

Publication title -

journal of robotics and mechatronics

Language(s) - English

Resource type - Journals

eISSN - 1883-8049

pISSN - 0915-3942

DOI - 10.20965/jrm.2016.p0928

Subject(s) - nonlinear system , inversion (geology) , avionics , supersonic speed , cruise , control theory (sociology) , flight control surfaces , cruise control , engineering , aerospace engineering , control system , cruise missile , control engineering , adaptive control , computer science , aerodynamics , control (management) , geology , artificial intelligence , missile , physics , paleontology , electrical engineering , quantum mechanics , structural basin

[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.

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