Paper Title:
Research on Attitude Law of Mass Moment Missile Based on Mulriple Control
  Abstract

Aimed at characteristics of mass moment of missiles in exo-atmosphere, it’s inferred that 6-DOF mathematical model based on mass moment controlling stabilities on three axes. Considering the problem of harmoniously controlling two moving masses, moving mass based non-linear theorem was used to solve a series of problems met in attitude control system design. In order to weaken the chattering of the system, a saturation function is introduced to substitute for Sign function to improve the variable structure control law so that the chattering can be depressed. The simulation results illustrate the efficiency of this method.

  Info
Periodical
Advanced Materials Research (Volumes 181-182)
Edited by
Qi Luo and Yuanzhi Wang
Pages
919-925
DOI
10.4028/www.scientific.net/AMR.181-182.919
Citation
P. Wu, Q. C. Chen, J. D. Ning, "Research on Attitude Law of Mass Moment Missile Based on Mulriple Control", Advanced Materials Research, Vols. 181-182, pp. 919-925, 2011
Online since
January 2011
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Price
$32.00
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