DocumentCode :
1752679
Title :
Modeling and Simulation of Endo-atmospheric Mass Moment Control Interceptor
Author :
Wang, Zhongkui ; Deng, Zongquan
Author_Institution :
Res. Center of Space Navigation Mechanism & Control, Harbin Inst. of Technol.
Volume :
1
fYear :
0
fDate :
0-0 0
Firstpage :
1843
Lastpage :
1847
Abstract :
In order to research endo-atmospheric mass moment control interceptor with three moving mass actuators, dynamics equations of this system are derived in detail. The dynamics model with nine degrees-of-freedom is presented. Then the integrated simulation is performed using SIMULINK without neglecting any control parameters. The important factors of influencing the angle-of-attack and angle-of-sideslip are found and the influence of negligible parameters to the system error is analyzed. Simulation results validate the feasibility of the mass moment control technique; and this will provide the basis for simplifying equations and the design of control system and moving mass actuators
Keywords :
actuators; aerospace control; control system analysis computing; control system synthesis; vehicle dynamics; control system design; dynamics equations; dynamics model; endo-atmospheric mass moment control interceptor; integrated simulation; moving mass actuators; Actuators; Automation; Control system synthesis; Control systems; Equations; Error analysis; Intelligent control; Navigation; Space technology; Weight control; mass moment interceptor; modeling; simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
Type :
conf
DOI :
10.1109/WCICA.2006.1712673
Filename :
1712673
Link To Document :
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