DocumentCode
3226081
Title
Block diagonal control for bank to turn winged missile
Author
Youan, Zhang ; Yunan, Hu
Author_Institution
Dept. of Autom. Control, Naval Aeronaut. Eng. Inst., Yantai, China
Volume
3
fYear
2002
fDate
28-31 Oct. 2002
Firstpage
1339
Abstract
The theory of block diagonal control (BDC) is applied to bank-to-turn (BTT) winged missile. The analytic inverse solutions of equations of the BTT missile are given. The BDC flight control system is constructed. To check the performance of the designed BDC control system, 6-DOF mathematical simulation is conducted. Simulation results show that the designed BDC can control the BTT missile stably and accurately.
Keywords
missile control; stability; BDC flight control system; BTT winged missile; analytic inverse solutions; bank-to-turn winged missile; block diagonal control; stability; Acceleration; Aerodynamics; Aerospace control; Aerospace simulation; Bandwidth; Control system synthesis; Control systems; Equations; Missiles; Nonlinear dynamical systems;
fLanguage
English
Publisher
ieee
Conference_Titel
TENCON '02. Proceedings. 2002 IEEE Region 10 Conference on Computers, Communications, Control and Power Engineering
Print_ISBN
0-7803-7490-8
Type
conf
DOI
10.1109/TENCON.2002.1182574
Filename
1182574
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