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Volume 35 Issue 11
Nov.  2009
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Journal of Beijing University of Aeronautics and Astronautics  > 2009  >  35(11): 1294-1297.
Yu Fuzhang, Cai Zhiyong, Hu Yingqionget al. Modeling of wireless datalink communication region between two aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(9): 1117-1120. (in Chinese)
Citation: Wu Yanshen, He Linshu. Attitude control technology of new-generation launch vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(11): 1294-1297. (in Chinese)
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Attitude control technology of new-generation launch vehicles

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 14 May 2008
  • Publish Date: 30 Nov 2009
    Abstract
  • A detail analysis was presented for attitude control design of new-generation launch vehicles. First, rigid body dynamics models and fluid sloshing dynamics models were developed based on Newton-Euler equations, and then elastic dynamics models which suggest a potential for interaction between attitude control and the structural dynamics of the vehicle, was investigated based on finite element method. According to dynamic models, attitude control system was designed. Toward the end, the method to reduce aerodynamics loads and fault tolerance design was aimed. In order to enhance the reliability of launch vehicle, fault-tolerant reconfiguration system was designed, and servo system fault influence on attitude control system was considered. Accelerometer feedback was used to reduce the aerodynamic lateral loads caused by in-flight atmospheric. All the results derived form above research are well suit for attitude control design of new-generation launch vehicles.

     

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  • [1] 杨云飞,李家文,陈宇,等.大型捆绑火箭姿态动力学模型研究[J].中国科学,2009,39(3):490-499 Yang Yunfei, Li Jiawen Chen Yu, et al. Research on attitude dynamics model of large launch vehicle[J]. Science in China,2009,39(3):490-499 [2] Loewy R G, Joglekar M M. Matrix holzer analysis for fully-coupled vibrations of clustered launch-vehicle configurations including applications to the Titan IIIC and uncoupled Saturn I cases . NASA CR-592, 1966 [3] 徐延万.液体弹道导弹与运载火箭系列-控制系统[M].北京:宇航出版社,1989 Xu Yanwan. Control system design of liquid propellant ballistic missile and launch Vechicle[M]. Beijing: China Astronautic Publishing House, 1989(in Chinese) [4] Mori H．Control system design of flexible-body launch vehicles[J].Control Engineering Practice, 1999,7,1163-1175
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