期刊文献+

单框架控制力矩陀螺部分失效时的空间站姿态机动方法 被引量:1

Space station attitude maneuver method considering partial fault of single gimbal control moment gyroscopes
下载PDF
导出
摘要 对金字塔构型单框架控制力矩陀螺(SGCMG)的失效特性进行分析。结合SGCMG部分失效的特点,构建运用Legendre伪谱法的重规划姿态机动路径求解方法。考虑SGCMG失效情况的不可预测性,设计自适应操纵律,该操纵律可以根据指令力矩与输出力矩的偏差对SGCMG的失效情况进行诊断,从而调节操纵律的内部参数,实现失效情况操纵律的自适应调节。仿真结果表明,采用姿态机动路径重规划算法与自适应操纵律,在控制力矩陀螺部分失效的情况下,仍可以实现空间站的大角度姿态机动。姿态机动方法可以有效应对空间站大角度姿态机动过程中可能出现的SGCMG部分失效情况,从而提高空间站姿态机动任务的安全性与可靠性。 The fault character of pyramid configuration single gimbal control moment gyroscopes (SGCMG) was analyzed. The calculation approach solving the replanned attitude maneuver path was proposed based on the Legendre pseudo spectral method. Considering the unpredictability of the SGCMG fault, an adaptive steering law was designed. Using this steering law, the fault state of SGCMG was detected and the parameters of the steering law was self-tuned. The simulation results reveal that, the large angle attitude maneuver can be accomplished by using the path replanned method and the adaptive steering law, when the SGCMG encounter partial fault. The proposed method can cope with the partial fault state of the SGCMG during attitude maneuver effectively, thus improving the security and reliability of the space station attitude maneuver mission.
作者 赵乾 唐国金
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 2015年第6期54-60,共7页 Journal of National University of Defense Technology
基金 国家自然科学基金资助项目(11272346) 国家973计划资助项目(2013CB733100)
关键词 姿态机动 控制力矩陀螺 路径规划 操纵律 attitude maneuver control moment gyroscopes path planning steering law
  • 相关文献

参考文献17

  • 1Fehse W. Automated rendezvous and docking of spacecraft[ M. UK: Cambridge University Press, 2003. 被引量:1
  • 2章胜,黄海兵,赵乾,唐国金.控制力矩陀螺辅助的空间站大角度姿态机动[J].国防科技大学学报,2013,35(4):7-13. 被引量:6
  • 3Bedrossian N, Bhatt S, Kang W, et al. Zero-propellant maneuver guidance J ]. IEEE Control System Magazine, 2009, 29(5) : 53 -73. 被引量:1
  • 4Bedrossian N, Bhatt S. First .ever flight demonstration of zero propellant maneuver ( TM ) attitude control concept [ C 5// Proceedings of AIAA Guidance, Navigation and Control Conference and Exhibit, 2007, AIAA 2007 - 6734 : 1 - 12. 被引量:1
  • 5Bedrossian N, Bhatt S, Lammers M, et al. Zero-propellant maneuver flight results for 180deg ISS rotation [ C ]// Proceedings of the 20th International Symposium on Space Flight Dynamics, 2008: 4833. 被引量:1
  • 6Kang W, Bedrossian N. Pseudospectral optimal control theory makes debut flight, saves NASA 1M dollars in under three hours[J], Society for Industrial and Applied Mathematics News, 2007, 40 (7) : 1 - 3. 被引量:1
  • 7Sands T A, Kim J J, Agrawal B N. Nonredundant single- gimbaled control moment gyroscopes [J]. Journal of Guidance Control and Dynamics, 2012, 35 (2) : 578 - 587. 被引量:1
  • 8Kasai S, Kojima H, Satoh M. Spacecraft attitude maneuver using two single-gimbal control moment gyros [ J 1. Acta Astronautica, 2013, 84:88-98. 被引量:1
  • 9Yamada K, Jikuya I, Kwak O. Rate damping of a spacecraft using two single-gimbal control moment gyros [ J]. Journal of Guidance Control and Dynamics, 2013, 36 ( 6 ) : 1606 - 1623. 被引量:1
  • 10Kwon S, Shimomura T, Okubo H. Pointing control of spacecraft using two SGCMGs via LPV control theory [ J ]. Acta Astronautica, 2011, 68(7) : 1168 -1175. 被引量:1

二级参考文献40

  • 1贾英宏,徐世杰,汤亮.Bias Momentum Attitude Control System Using Energy/Momentum Wheels[J].Chinese Journal of Aeronautics,2004,17(4):193-199. 被引量:6
  • 2Margulies G, Aubrun J N. Geometric theory of single-gimbal control moment gyro systems[J]. Journal of the Astronautical Sciences, 1978, 26(2): 159-191. 被引量:1
  • 3Dominguez J, Wie B. Computation and visualization of control moment gyroscope singularities[R]. AIAA-2002-4570, 2002. 被引量:1
  • 4Wie B. Singularity analysis and visualization for single-gimbal control moment gyro systems[J]. Journal of Guidance, Control and Dynamics, 2004, 27(2): 271-282. 被引量:1
  • 5Kurokawa H. A geometry study of single gimbal control moment gyros-singularity problem and steering law[R]. Technical Report of Mechanical Engineering Laboratory TR-175, Tsukuba: Mechanical Engineering Lab, 1998. 被引量:1
  • 6Yoon H,Tsiotras P. Singularity analysis of variable-speed control moment gyros[J]. Journal of Guidance, Control and Dynamics, 2004, 27(3): 374-386. 被引量:1
  • 7Hanspeter S, John L J. Singularity avoidance using null motion and variable-speed control moment gyros[J]. Journal of Guidance, Control and Dynamics, 2000, 23(1): 11-16. 被引量:1
  • 8Yoon H, Tsiotras P. Spacecraft adaptive attitude and power tracking with variable speed control moment gyroscopes[J]. Journal of Guidance, Control and Dynamics, 2002, 25(6): 1081-1090. 被引量:1
  • 9Tang L, Xu S J. Integrated power and attitude control using VSCMGs for agile satellite[A]. In: Vladimir P ed. Proceedings of 16th IFAC Symposium on Automatic Control in Aerospace[C]. St Petersburg: Elsevier, 2004. 被引量:1
  • 10Bedrossian N B, Paradiso J, Bergmann E V. Redundant single gimbal control moment gyroscope singularity analysis[J]. Journal of Guidance, Control and Dynamics, 1990, 13(6): 1083-1089. 被引量:1

共引文献43

同被引文献11

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部