Design of the nonlinear structure adaptive model inversion flight control system

Hao Long, Yi-Nung Chung

Research output: Contribution to journalArticle

1 Citation (Scopus)

Abstract

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 multisubsystem 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.

Original languageEnglish
Pages (from-to)928-935
Number of pages8
JournalJournal of Robotics and Mechatronics
Volume28
Issue number6
Publication statusPublished - 2016 Dec 1

Fingerprint

Flight control systems
Aircraft
Nonlinear control systems
Maneuverability
Avionics
Takeoff
Landing
Control systems

All Science Journal Classification (ASJC) codes

  • Computer Science(all)
  • Electrical and Electronic Engineering

Cite this

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Design of the nonlinear structure adaptive model inversion flight control system. / Long, Hao; Chung, Yi-Nung.

In: Journal of Robotics and Mechatronics, Vol. 28, No. 6, 01.12.2016, p. 928-935.

Research output: Contribution to journalArticle

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