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运载火箭初始对准仿真系统的研究 被引量:1

The Study of Launch Vehicle Platform Align Emulation System
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摘要 本文讨论并建立了运载火箭初始对准系统的物理数学模型,并用多媒体手段对系统实际工作过程进行了仿真模拟。结果表明,仿真系统完全满足训练要求。 Physical and mathematical model for the inertia1 platform initialization align system of launch vehicle is discussed in this paper. By means of multimedia, the operating process of the system is emulated. The results are satisfied for training purpose.
出处 《指挥技术学院学报》 1999年第1期38-42,共5页 Journal of Institute of Command and Technology
关键词 惯性平台 初始对准 仿真 运载火箭 对准 制导 inertial platform initialization align digital emulation
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  • 1Fezans N,Alazard D, Imbert N, et al. H (infinity) control design for multivariable mechanical systems - Application to RLV reentry [ C ]. AIAA Guidance, Navigation, and Control Conference Proceedings and Exhibit, South Carolina, USA, August 1 -13, 2007.
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  • 7徐骋,强文义,王长青.基于逆动力学的飞行器直接力控制系统及其稳定性分析[J].宇航学报,2008,29(4):1308-1313. 被引量:4
  • 8杨炳渊,樊则文.弹性飞行器气动伺服弹性耦合动力学仿真[J].宇航学报,2009,30(1):134-138. 被引量:8
  • 9杨云飞,李家文,陈宇,程堂明,赵育善.大型捆绑火箭姿态动力学模型研究[J].中国科学(E辑),2009,39(3):490-499. 被引量:21
  • 10彭蓉,严恭敏,秦永元.箭载捷联惯导系统水平自对准的两种实用方法[J].中国惯性技术学报,2009,17(4):428-435. 被引量:6

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