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| 太阳帆航天器被动姿态控制研究 | |
| 引用本文： | 骆军红,李晓东,冯军华. 太阳帆航天器被动姿态控制研究[J]. 飞行力学, 2008, 26(5) |
| 作者姓名： | 骆军红 李晓东 冯军华 |
| 作者单位： | 1. 中国空空导弹研究院,人力资源部,河南,洛阳,471009 2. 中国地质大学,地球科学与资源学院,北京,100083 3. 哈尔滨工业大学飞行器动力学与控制研究所,黑龙江,哈尔滨,150080 |
| 基金项目： | 国家863计划资助项目(2005AA737071) |
| 摘 要： | 针对由有效载荷、太阳帆和4个控制叶片所组成的太阳帆航天器系统,从物理模型出发,利用欧拉方程建立了姿态动力学模型,并通过数值仿真对太阳帆航天器基于控制叶片的对日定向性能进行了研究。研究结果表明,在行星际飞行中太阳帆航天器可以通过使控制叶片保持偏置来保持姿态稳定。 |
| 关 键 词： | 动力学建模 姿态控制 太阳帆航天器 控制叶片 |
Passive Attitude Control of Solar Sail Spacecraft |
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| LUO Jun-hong,LI Xiao-dong,FENG Jun-hua. Passive Attitude Control of Solar Sail Spacecraft[J]. Flight Dynamics, 2008, 26(5) | |
| Authors: | LUO Jun-hong LI Xiao-dong FENG Jun-hua |
| Affiliation: | 1.Human Resource Department;China Airbome Missile Academy;Luoyang 471009;China;2.School of the Earth Sciences and Resources;China University of Geosciences;Beijing 100083;3.Institute of Aerocraft Dynamics and Control;Harbin Institute of Technology;Harbin 150080;China |
| Abstract: | A solar sail spacecraft which is composed of four parts-sail film,structural booms,and payload mass,control vanes was studied.Dynamic model of the solar sail spacecraft was established using the Euler equation.Then,the nonlinear rotation system was run through a series of simulations to characterize the behavior of passive attitude control using control vanes and determine the effectiveness of attitude controlling.Results of simulations showed that the solar sail spacecraft could be stable in the present of... |
| Keywords: | dynamics modeling attitude control solar sail spacecraft control vane |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |