Paper Title:
Research of De-Couple Control System for near Space Vehicle with High Maneuver and Couple
  Abstract

A de-couple control method with information feedback from other control channel and a method with double control loops were present for the hypersonic vehicle with non-linear, couple and lateral maneuver. The whole controller was divided into two parts: the computation of actuator which deal with control couple and design of control law which solve the problem of movement and aerodynamic couple. The time-varying controller parameter method and robust control law were present to solve the problem of quick time-varying model parameter and non-linear. Finally these two methods were analyzed contrastively; the simulation result show that these two methods present above can achieve the quick dynamic and high precise track of command. But the latter was better.

  Info
Periodical
Chapter
Chapter 4: Fault Diagnose and Electronmechanical Control
Edited by
Zhixiang Hou
Pages
979-984
DOI
10.4028/www.scientific.net/AMM.128-129.979
Citation
S. B. Ni, W. J. Hu, S. Xiong, "Research of De-Couple Control System for near Space Vehicle with High Maneuver and Couple", Applied Mechanics and Materials, Vols. 128-129, pp. 979-984, 2012
Online since
October 2011
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