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
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;
Conference_Titel :
TENCON '02. Proceedings. 2002 IEEE Region 10 Conference on Computers, Communications, Control and Power Engineering
Print_ISBN :
0-7803-7490-8
DOI :
10.1109/TENCON.2002.1182574
