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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1999, Vol. 20 ›› Issue (5): 475-477.

• 论文 • Previous Articles     Next Articles

LAYERED SLIDING MODEL CONTROL OF THE AERODYNAMIC MISSILE

WEI Feng1, ZHANG Fu-en1, GU Wen-jing2, YAO Hong2   

  1. 1. Department of Automatic Control, Harbin Institute of Technology, Harbin 150001, China;2. Department of Automatic Control, Naval Aerodynamic Engineering Academy, Yantai 264001, China
  • Received:1998-09-09 Revised:1999-02-28 Online:1999-10-25 Published:1999-10-25

Abstract: The model of the areodynamic missile can be described as a block diagonal construction with four layers.After getting an affine form of 1st and 2nd layers,an affine form with four layers of the missile is gotten in this paper.By using the form, this paper develops a procedure called sliding model block diagonal controller, which realizes a design of a nonlinear system of a missile. The simulation shows that the procedure has a powerful robustness for the model.

Key words: areodynam ic m issile, cont ro l system, block diagonal, layered sliding model cont ro l

CLC Number: