As an innovative passive deorbit technology,electrodynamic tethered(EDT)deorbit technology is applicable to the upper-stage of launch vehicles,due to its low fuel cost and high efficiency.The present paper deals with the dynamic modeling and control problem of EDT upper-stage deorbit system.To this end,based on mission analysis,we conduct dynamic modeling and practical control scheme design for tether deployment and deorbit phase,respectively.Numerical simulations are given to validate the effectiveness of the proposed control schemes.Finally,a brief remark on state-of-the-art flight test and ground experiments is helpful for the future development of EDT deorbit technology.
ZHANG Feng
,
WANG Xiao-ding
,
WANG Chang-qing
,
KONG Ling-chao
,
WU Sheng-bao
. Dynamics and Control for Electrodynamic Tethered Upper-Stage Deorbit System[J]. Journal of Space Science and Experiment, 2021
, 21(3)
: 9
-19
.
DOI: 10.19963/j.cnki.2096-4099.2021.03.002
[1] Shan M,Guo J,Gill E.Review and comparison of active space debris capturing and removal methods[J].Progress in Aerospace Sciences,2016,80:18—32.
[2] 江海,刘静.空间碎片与空间交通管理[J].空间碎片研究,2019,19(1):39—44.
[3] 王小锭,张烽,申麟,等.空间平台电动力绳系离轨装置技术研究[J].空间碎片研究,2020,20(2):22—31.
[4] Rouleau G,Verma S,Sharf I,et al.Vision-based tracking and trajectory generation for robotic capture of objects in space[C].California:AIAA Guidance,Navigation and Control Conference,2005.
[5] 李懿德,范鑫.PW-Sat2立方星离轨帆研制及在轨验证[J].航天器环境工程,2020,37(4):414—420.
[6] Sanmartin J R,Lorenzini E C,Martinez-Sanchez M.Electrodynamic tether applications and constraints[J].Journal of Spacecraft and Rockets,2010,47(3):442—456.
[7] Zhang F,Performance and applicability of orbital transfer with bare electrodynamic tether[J].Journal of Spacecraft and Rockets,2019,56(1):21—32.
[8] 王小锭,张烽,董晓琳,等.基于电动力绳的火箭末级离轨系统设计及效能分析[J].导弹与航天运载技术,2018,2:13—19.
[9] Wen H,Jin D,Hu H,Advances in dynamics and control of tethered satellite systems[J].Acta Mechanica Sinica,2008,24(3):229—241.
[10] Wen H,Zhu Z H,Jin D P,et al.Model predictive control with output feedback for a deorbiting electrodynamic tether system[J].Journal of Guidance,Control,and Dynamics,2016,39(10):2451—2456.
[11] 余本嵩,金栋平,庞兆君.绳系释放时的航天器耦合动力学分析[J].中国科学:物理力学天文学,2014,44(8):858—964.
[12] 张烽,王小锭,王书廷,等.火箭末级离轨系统中电动力绳系释放条件分析与控制设计[J].宇航总体技术,2021,5(2):1—6.
[13] Zhang Feng,Shen Lin,Wu Shengbao,et al.Elec-trodynamic tethered deorbit system dynamics[J].Aerospace China,2016,17(3):1—11.
[14] 张烽,申麟,吴胜宝,等.电动力绳系离轨技术性能与任务适应性分析[J].导弹与航天运载技术,2017,3:6—11.
[15] Sanmartin J,Martinez-Sanchez M,Ahedo E.Bare wire anodes of electrodynamic tethers[J].Journal of Propulsion and Power,1993,9(3):353—360.
[16] Zhong R,Zhu Z H.Dynamics of nanosatellite deorbit by bare electrodynamic tether in low earth orbit[J].Journal of Spacecraft and Rocket,2013,50(3):691—700.
[17] 陈辉,文浩,金栋平,等.绳系卫星在轨试验及地面物理仿真进展[J].力学进展,2013,43(1):174—184.
[18] 余本嵩,文浩,金栋平,等.空间电动力绳系统理论及实验研究[J].力学进展,2016,46(1):226—266.
[19] 李爱军,李艳芳,王长青,等.电动力系绳离轨系统关键技术简析[J].航天器环境工程,2020,37(4):323—329.
[20] 张烽,王小锭,吴胜宝,等,日本KITE试验任务综述与启示,空间碎片研究,2018,18(2):23—32.
