| 引用本文: | 赵亚飞,张世杰,过佳雯,孙俊,曹喜滨.考虑飞轮动力学的过驱动卫星控制分配算法[J].哈尔滨工业大学学报,2013,45(7):1.DOI:10.11918/j.issn.0367-6234.2013.07.001 |
| ZHAO Yafei,ZHANG Shijie,GUO Jiawen,SUN Jun,CAO Xibin.Dynamic control allocation for overactuated satellite with flywheel dynamics[J].Journal of Harbin Institute of Technology,2013,45(7):1.DOI:10.11918/j.issn.0367-6234.2013.07.001 |
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| 摘要: |
| 针对具有冗余飞轮的过驱动卫星的最优控制分配问题,以反作用飞轮总能耗和力矩分配偏差最小等为目标,通过定义与能耗相关的优化目标函数,提出了能耗/力矩优化的动态控制分配方法,并考虑飞轮的非线性动力学特性,对控制分配进行修正．最后对本文提出的控制分配算法进行了数学仿真验证,结果表明了上述方法的可行性和有效性． |
| 关键词: 过驱动卫星 控制分配 反作用飞轮 动力学 |
| DOI：10.11918/j.issn.0367-6234.2013.07.001 |
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| 基金项目:国家自然科学基金资助项目(60704020). |
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| Dynamic control allocation for overactuated satellite with flywheel dynamics |
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ZHAO Yafei1, ZHANG Shijie1, GUO Jiawen1, SUN Jun1,2, CAO Xibin1
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(1. Research Center of Satellite Technology, Harbin Institute of Technology, 150080 Harbin, China;2. Shanghai Key Laboratory of Space Intelligent Control Technology, 200233 Shanghai, China)
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| Abstract: |
| Considering overactuated satellite optimal control allocation problem with redundant reaction wheels, in order to achieve minimum total energy consumption and torque allocation deviation as a goal, an energy/torque dynamic control allocation algorithm is proposed by defining relevant optimized objective function. Also, the proposed method takes nonlinear dynamics into account and modifies the initial control allocation result. Finally, mathematical simulations are used to verify the performance of the algorithm, the result shows its feasibility and effectiveness. |
| Key words: overactuated satellite control allocation reaction flywheels dynamics
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