期刊文献+

绳系卫星渐近稳定释放与回收策略 被引量:3

Asymptotic Stabilization for Deployment and Retrieval of a Tethered Satellite System
下载PDF
导出
摘要 文章研究椭圆轨道下绳系卫星的稳定释放与回收控制问题。首先基于Lyapunov稳定性理论,获得椭圆轨道下系绳释放和回收的速率控制律及稳定性条件,然后提出一套能使系绳沿期望俯仰角进行渐近稳定释放和回收控制的方法。指出存在一个轨道区间,可以实现对通常不稳定的回收过程进行稳定回收,进而提出分区间和分段回收策略以优化回收控制效果。最后,通过数值模拟对所提出的控制律、稳定条件及控制策略进行验证。 An asymptotic stability strategy for deployment and retrieval of a tethered satellite system in elliptical orbits was studied Firstly, the stability of an in-plane tethered satellite system moving in an elliptical orbit was analyzed, a novel rate control for stabilizing the deployment and retrieval was obtained, and the stability conditions for the control were given based on Lyapunov stability theory. Then, a rate-based control method to suppress the large swing around the local vertical position of tethered satellite system was presented. Under such control strategy, the deployment and retrieval of the tether made an asymptotic stable motion towards to the preassigned pitch angle. The results show that there exists an orbital region, on which the retrieval process can keep asymptotic stability. To optimize the effect of retrieval control, the partitioning and segmenting strategies Finally, the proposed control law, stability conditions, demonstrated by the numerical simulations. on the orbit were proposed. and control strategies were
出处 《中国空间科学技术》 EI CSCD 北大核心 2013年第5期35-42,共8页 Chinese Space Science and Technology
基金 国家自然科学基金(50875124 11202094) 长江学者和创新团队计划(IRT0968) 中国博士后科学基金(2012M521070) 中央高校基本科研业务费专项资金(NS2012034)资助项目
关键词 释放 回收 控制律 稳定条件 绳系卫星 Deployment Retrieval Control law Stability condition Tethered satellite
  • 相关文献

参考文献11

  • 1DJEBLI A, EL BAKKALI L, PASCAL M. On fast retrieval laws for tethered satellite systems [J]. Acta Astronautica, 2002, 50(8): 461-470.
  • 2BARKOW B, STEINDL A, TROGER H, et al. Various methods of controlling the deployment of a tethered satellite [J]. Journal of Vibration and Control, 2003, 9(1): 187-208.
  • 3NAKAMURA Y, HASHIMOTO H. Ground test of tether deployment and retrieval along optimal path with a tether reeling mechanism designed for micro-class satellites [C]. The 54th International Astronautical Congress, Bremen: International Astronautical Federation, 2003.
  • 4BARKOW B, STEINDL A, TROGER H. A targeting strategy for the deployment of a tethered satellite system [J]. IMA Journal of Applied Mathematics, 2005, 70(5): 626-644.
  • 5MANTRI P, MAZZOLENI A P, PADGETT D A. Parametric study of deployment of tethered satellite systems [J]. Journal of Spacecraft and Rockets, 2007, 44(2): 412-424.
  • 6WILLIAMS P. Deployment/retrieval optimization for flexible tethered satellite systems [J]. Nonlinear Dynamics, 2008, 52(1-2): 159-179.
  • 7SANMARTIN J R, LORENZINI E C, MARTINEZ-SANCHEZ M. Electrodynamic tether applications and constraints [J]. Journal of Spacecraft and Rockets, 2010, 47(3): 442-456.
  • 8YU B S, JIN D P. Deployment and retrieval of tethered satellite system under J2 perturbation and heating effect [J]. Acta Astronautica, 2010, 67(7 8): 845 853.
  • 9LIU Y Y, ZHOU J, CHEN H L. Variable structure control for tethered satellite fast deployment and retrieval [J]. Future Control and Automation, 2012, 172(1): 157-164.
  • 10JIN D P, HUH Y. Optimal control of a tethered subsatellite of three degrees of freedom [J]: Nonlin- ear Dynamics, 2006, 46(1-2) 161-178.

同被引文献11

引证文献3

二级引证文献2

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