1 |
张玉锟.卫星编队飞行的动力学与控制技术研究[D].长沙: 国防科学技术大学, 2002.
|
|
ZHANG Y K. Research on dynamics and control of satellite formation flying[D]. Changsha: National University of Defense Technology, 2002.
|
2 |
GOU X W , LI A J , TIAN H C , et al. Overload control of artificial gravity facility using spinning tether system for high eccentricity transfer orbits[J]. Acta Astronautica, 2018, 147, 383- 392.
doi: 10.1016/j.actaastro.2018.03.005
|
3 |
SHI G F , ZHU Z X , ZHU Z H . Stable orbital transfer of partial space elevator by tether deployment and retrieval[J]. Acta Astronautica, 2018, 152, 624- 629.
doi: 10.1016/j.actaastro.2018.09.013
|
4 |
KHAN B S , SANMARTIN J R . Analysis of tape tether survival in LEO against orbital debris[J]. Advances in Space Research, 2014, 53 (9): 1370- 1376.
doi: 10.1016/j.asr.2014.02.008
|
5 |
孟中杰, 黄攀峰, 鲁迎波, 等. 在轨服务中空间系绳的应用及发展[J]. 宇航学报, 2019, 40 (10): 1134- 1145.
|
|
MENG Z J , HUANG P F , LU Y B , et al. Applications and development of space tether in on-orbit servicing[J]. Journal of Astronautics, 2019, 40 (10): 1134- 1145.
|
6 |
WILLIAMS P , BLANKSBY C , TRIVAILO P . Tethered planetary capture: controlled maneuvers[J]. Acta Astronautica, 2003, 53, 681- 708.
doi: 10.1016/S0094-5765(03)80029-2
|
7 |
DIAKOV P A , MALASHIN A A , SMIRNOV N N . Dynamic processes in the tether of a space tethered system[J]. Acta Astronautica, 2019, 163, 100- 106.
doi: 10.1016/j.actaastro.2019.01.019
|
8 |
SUN L , GUO W Z , HUANG H , et al. Optimal control scheme of the tethered system for orbital transfer under a constant thrust[J]. International Journal of Aerospace Engineering, 2018, 1572726.
|
9 |
YU S H , WEN H , JIN D P . Review of deployment technology for tethered satellite systems[J]. Acta Mechanica Sinica, 2018, 34 (4): 754- 768.
doi: 10.1007/s10409-018-0752-5
|
10 |
YU S H . Dynamic model and control of mass-distributed tether satellite system[J]. Journal of Spacecraft and Rockets, 2002, 39 (2): 213- 218.
doi: 10.2514/2.3822
|
11 |
LIAO Y X , LI H F , BAO W M . Indirect Radau pseudospectral method for the receding horizon control problem[J]. Chinese Journal of Aeronautics, 2016, 29 (1): 215- 227.
doi: 10.1016/j.cja.2015.12.023
|
12 |
OHTSUKA T , FUJⅡ H A . Real-time receding-horizon control algorithm for nonlinear systems[J]. Transactions of the Society of Instrument & Control Engineers, 1997, 33 (12): 1131- 1139.
|
13 |
FUJⅡ H A , ANAZAWA S . Deployment/ retrieval control of tethered subsatellite through an optimal path[J]. Journal of Guidance, Control, and Dynamics, 1994, 17 (6): 1292- 1298.
doi: 10.2514/3.21347
|
14 |
KOKUBUN K , ANAZAWA S , FUJⅡ H A . Real-time optimal state feedback control for tethered subsatellite system[J]. Journal of Guidance, Control, and Dynamics, 1996, 19 (4): 972- 974.
doi: 10.2514/3.21728
|
15 |
WILLIAMS P . Deployment/retrieval optimization for flexible tethered satellite systems[J]. Nonlinear Dynamics, 2008, 52 (1): 159- 179.
|
16 |
MA Z Q , SUN G H . Adaptive sliding mode control of tethered satellite deployment with input limitation[J]. Acta Astronautica, 2016, 127, 67- 75.
doi: 10.1016/j.actaastro.2016.05.022
|
17 |
CHU Z Y , DI J N , CUI J . Hybrid tension control method for tethered satellite systems during large tumbling space debris removal[J]. Acta Astronautica, 2018, 152, 611- 623.
doi: 10.1016/j.actaastro.2018.09.016
|
18 |
HU Y X , HUANG P F , MENG Z J , et al. Optimal control of approaching target for tethered space robot based on non-singular terminal sliding mode method[J]. Advances in Space Research, 2019, 63 (12): 3848- 3862.
doi: 10.1016/j.asr.2019.02.034
|
19 |
WANG C , ZHANG F . Finite-time stability of an underactuated tethered satellite system[J]. Acta Astronautica, 2019, 159, 199- 212.
doi: 10.1016/j.actaastro.2019.03.044
|
20 |
SUN L , ZHAO G W , HUANG H . Stability and control of tethered satellite with chemical propulsion in orbital plane[J]. Nonlinear Dynamics, 2013, 74 (4): 1113- 1131.
doi: 10.1007/s11071-013-1028-z
|
21 |
LI P J , ZHONG R , LU S . Optimal control scheme of space tethered system for space debris deorbit[J]. Acta Astronautica, 2019, 165, 355- 364.
doi: 10.1016/j.actaastro.2019.09.031
|
22 |
RAZZAGHI P , Al KHATIB E , BAKHTIARI S . Sliding mode and SDRE control laws on a tethered satellite system to de-orbit space debris[J]. Advances in Space Research, 2019, 64 (1): 18- 27.
doi: 10.1016/j.asr.2019.03.024
|
23 |
LIU J Y , LI G Q , ZHU Z H , et al. Orbital boost characteristics of spacecraft by electrodynamic tethers with consideration of electric-magnetic-dynamic energy coupling[J]. Acta Astronautica, 2020, 171, 196- 207.
doi: 10.1016/j.actaastro.2020.03.001
|
24 |
KUMAR K D . Review of dynamics and control of nonelectrodynamic tethered satellite systems[J]. Journal of Guidance, Control and Dynamics, 2006, 43 (4): 705- 720.
|
25 |
唐国金, 罗亚中, 雍恩米. 航天器轨迹优化理论、方法及应用[M]. 北京: 科学出版社, 2012.
|
|
TANG G J , LUO Y Z , YONG E M . Theory, method and application of spacecraft trajectory optimization[M]. Beijing: Science Press, 2012.
|
26 |
PIMNOO A , HIRAKI K . Relative dynamics and motion control of nanosatellite formation flying[J]. Advances in Space Research, 2016, 57 (7): 1476- 1493.
doi: 10.1016/j.asr.2016.01.004
|
27 |
曹喜滨, 张锦绣, 弗拉基米尔·阿斯拉诺夫, 等. 绳系卫星系统动力学[M]. 北京: 国防工业出版社, 2015.
|
|
CAO X B , ZHANG J X , ASLANOV V S , et al. Dynamics of tethered satellite systems[M]. Beijing: National Defense Industry Press, 2015.
|
28 |
PATTERSON M A , RAO A V . GPOPS-Ⅱ: a Matlab software for solving multiple-phase optimal control problems using hp-adaptive Gaussian quadrature collocation methods and sparse nonlinear programming[J]. ACM Trans.on Mathematical Software, 2010,, 41 (1): 1- 37.
|
29 |
BEVILACQUA F , MERLINA P , CIARDO S . Tethered space elevator possible applications & demonstrative experiments[J]. Acta Astronautica, 1988, 18, 73- 82.
doi: 10.1016/0094-5765(88)90089-6
|
30 |
ZHANG J , WANG X , MA X B , et al. Spacecraft long-duration phasing maneuver optimization using hybrid approach[J]. Acta Astronautica, 2012, 72, 132- 142.
doi: 10.1016/j.actaastro.2011.09.008
|