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