Paper Title:
Stable Nonlinear Control Allocation for Aircraft with Multiple Control Effectors
  Abstract

With respect to aircraft with redundant multiple control effectors, a nonlinear controller, which is composed of a virtual control law and a dynamic control allocation with position constraints of each effector, is designed. Based on Lyapunov stability theory and LaSalle invariant set theorem, asymptotic stabilities of upper control subsystem, dynamic control allocation subsystem and overall closed-loop system are proved respectively. Simulation results show the effectiveness of the proposed method.

  Info
Periodical
Chapter
Chapter 1: Applied Mechanics Mechanical Engineering
Edited by
Honghua Tan
Pages
404-409
DOI
10.4028/www.scientific.net/AMM.138-139.404
Citation
H. Li, J. Y. Yu, Y. A. Zhang, "Stable Nonlinear Control Allocation for Aircraft with Multiple Control Effectors", Applied Mechanics and Materials, Vols. 138-139, pp. 404-409, 2012
Online since
November 2011
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