Paper Title:
Supersonic Missile Control with PI Sliding Mode Method
  Abstract

Comparing with traditional adaptive methods, a very simple PI sliding mode controller is designed for uncertain nonlinear missile systems with the help of two main assumptions which are also testified to be reasonable.The construction of PI control for sliding surface is novel and effective. Also, the proof of PI type control law is unique in this paper.

  Info
Periodical
Advanced Materials Research (Volumes 295-297)
Chapter
Chapter 4: Material Removal Processes and Machines
Edited by
Pengcheng Wang, Liqun Ai, Yungang Li, Xiaoming Sang and Jinglong Bu
Pages
1773-1776
DOI
10.4028/www.scientific.net/AMR.295-297.1773
Citation
Q. Ma, Y. Q. Jin, "Supersonic Missile Control with PI Sliding Mode Method", Advanced Materials Research, Vols. 295-297, pp. 1773-1776, 2011
Online since
July 2011
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Price
$32.00
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