| 基于改进姿态控制系统模型的卫星多学科优化 |
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| 引用本文： | 王晓峰,黄海.基于改进姿态控制系统模型的卫星多学科优化[J].航空动力学报,2007,22(11):1958-1962. |
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| 作者姓名： | 王晓峰 黄海 |
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| 作者单位： | 北京航空航天大学,宇航学院,北京,100083 |
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| 摘 要： | 分析了三轴稳定卫星姿态控制分系统与其它分系统的耦合关系,选定了姿态稳定方式和姿态控制系统硬件,建立了更为精确的计算姿态控制分系统质量和功率的分析模型,然后基于多学科设计优化协同优化算法建立了总体系统、姿态控制分系统、电源分系统和结构分系统的优化模型,最后用C语言对分析模型和优化模型编程计算.结果表明,分系统模型能与总体系统模型有效协调优化,得到更好的总体性能指标.
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| 关 键 词： | 航空航天推进系统 姿态控制 卫星 多学科优化设计 建模 改进 姿态控制 系统模型 卫星姿态 多学科优化 attitude control system satellite model advanced based 性能指标 协调优化 结果 编程计算 语言对 优化模型 结构 电源分系统 优化算法 多学科设计优化 |
| 文章编号： | 1000-8055(2007)11-1958-05 |
| 收稿时间： | 2006/10/24 0:00:00 |
| 修稿时间： | 2006年10月24 |
Multidisciplinary design optimization based on advanced model of satellite attitude control system |
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| WANG Xiao-feng and HUANG Hai.Multidisciplinary design optimization based on advanced model of satellite attitude control system[J].Journal of Aerospace Power,2007,22(11):1958-1962. |
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| Authors: | WANG Xiao-feng and HUANG Hai |
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| Institution: | School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
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| Abstract: | The coupled relationship between the attitude control system and other subsystems of three-axis-stabilized satellite was analyzed in this paper,and then attitude control models and subsystem hardware were selected.More accurate analysis model was established to calculate subsystem mass and power,then optimization models of integrated system,attitude control subsystem,power subsystem and structure subsystem based on collaborative optimization(CO) methodology were built. Finally,the programs were compiled with C language for the analysis models and optimization models.The results shows: subsystem model collaborates well with this system model to obtain better system performance. |
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| Keywords: | aerospace propulsion system attitude control satellite multidisciplinary design optimization(MDO) model |
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