Method of SLAS’s ground track manipulation based on tangential impulse thrust

doi:10.23919/JSEE.2023.000125

Journal of Systems Engineering and Electronics ›› 2023, Vol. 34 ›› Issue (5): 1285-1293.doi: 10.23919/JSEE.2023.000125

收稿日期:2022-09-26 出版日期:2023-10-18 发布日期:2023-10-30

Method of SLAS’s ground track manipulation based on tangential impulse thrust

Xinlong LE(), Xibin CAO(), Yu DAI(), Fan WU()

¹ School of Astronautics, Harbin Institute of Technology, Harbin 150001, China

Received:2022-09-26 Online:2023-10-18 Published:2023-10-30
Contact: Fan WU E-mail:xinlong_le@163.com;xbcao@hit.edu.cn;daiyu2677@163.com;wufanrcst@hit.edu.cn
About author:
LE Xinlong was born in 1999. He received his B.E. degree from Harbin Institute of Technology. He is pursuing his Ph.D. degree in Harbin Institute of Technology. His research interests are satellite formation, satellite orbit control. E-mail: xinlong_le@163.com

CAO Xibin was born in 1963. He received his Ph.D. degree from Harbin Institute of Technology. He is a professor in Harbin Institute of Technology. He was selected as an Academician of Chinese Academy of Engineering, in 2019. His research interests include system design of spacecraft and system simulation. E-mail: xbcao@hit.edu.cn

DAI Yu was born in 2000. He is currently pursuing his B.E degree in the School of Astronautics, Harbin Institute of Technology. He is currently pursuing his M.S. degree in Harbin Institute of Technology. His research interest is in-orbit space environment. E-mail: daiyu2677@163.com

WU Fan was born in 1993. He received his B.E., M.S., and Ph.D. degrees from Harbin Institute of Technology. He is an associate professor in Harbin Institute of Technology. His research interests include spacecraft attitude dynamics and control and system design. E-mail: wufanrcst@hit.edu.cn
Supported by:
The work was supported by the National Natural Science Foundation of China (11972130) and the Heilongjiang Touyan Team Program (11972130)

摘要/Abstract

Abstract:

Satellites with altitudes below 400 km are called super low altitude satellites (SLAS), often used to achieve responsive imaging tasks. Therefore, it is important for the manipulation of its ground track. Aiming at the problem of ground track manipulation of SLAS, a control method based on tangential impulse thrust is proposed. First, the equation of the longitude difference between SLAS and the target point on the target latitude is derived based on Gauss’s variational equations. On this basis, the influence of the tangential impulse thrust on the ground track’s longitude is derived. Finally, the method for ground track manipulation of SLAS under the tangential impulse thrust is proposed. The simulation results verify the effectiveness of the method, after manipulation, the satellite can visit the target point and revisit it for multiple days.

Key words: super low altitude satellite (SLAS), ground track drift modeling, ground track manipulation, tangential impulse thrust

. [J]. Journal of Systems Engineering and Electronics, 2023, 34(5): 1285-1293.

Xinlong LE, Xibin CAO, Yu DAI, Fan WU. Method of SLAS’s ground track manipulation based on tangential impulse thrust[J]. Journal of Systems Engineering and Electronics, 2023, 34(5): 1285-1293.

图/表 12

参考文献 23

1	NAGANO H, KAJIWARA K, OSUGA H, et al Research and development of a new power processing control unit of ion engine system for the super low altitude test satellite. Transactions of The Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 2011, 8 (27): 17- 22.
2	KIMOTO Y, YUKUMATSU K, GOTO A, et al MDM: a flight mission to observe materials degradation in-situ on satellite in super low Earth orbit. Acta Astronautica, 2021, 179, 695- 701. doi: 10.1016/j.actaastro.2020.11.048
3	HU Y P, LI K B, LIANG Y G, et al Review on strategies of space-based optical space situational awareness. Journal of Systems Engineering and Electronics, 2021, 32 (5): 1152- 1166.
4	YUAN C Z, ZHANG Q, FU D Y, et al Super-low orbit satellite technology development and prospects. Spacecraft Engineering, 2021, 30 (6): 89- 99.
5	KUIJPER D, MATATOROS M A G Goce flight dynamics operations from an orbital perspective. Journal of Aerospace Engineering, Sciences and Applications, 2012, 2 (4): 93- 106.
6	ATSUSHI N, MASANORI H, MASAYOSHI U. The study of a super low altitude satellite. Transactions of Space Technology Japan, 2009, 7(26): 17−22.
7	VAN A, RICHARD E, JAMES R W NanoEye-a multi-mission low cost spacecraft. Proc. of the Reinventing Space Conference, 2012, 8- 11.
8	FU X F. Orbit design in responsive space missions. Changsha: National University of Defense Technology, 2012. (in Chinese)
9	MENG S F, SHU J S, YANG Q, et al Analysis of detection capabilities of LEO reconnaissance satellite constellation based on coverage performance. Journal of Systems Engineering and Electronics, 2018, 29 (1): 98- 104.
10	YANG Y A, FENG Z R, SUN L Y, et al Shift control method for the local time at descending node based on sun-synchronous orbit satellite. Journal of Systems Engineering and Electronics, 2009, 20 (1): 141- 145.
11	WEN S L, YAN Y, YI T Analyzing perturbation characteristic and orbital maintenance strategy for super low altitude satellite. Journal of National University of Defense Technology, 2015, 37 (2): 128- 134.
12	WEN S L Dynamic modeling and flight control for super low altitude satellite. Changsha: National University of Defense Technology, 2016.
13	YANG S Q, DU Y K, CHEN J L Design of strictly-regressive orbit based on iterative adjustment method. Journal of Astronautics, 2016, 37 (4): 420- 426.
14	MASAYOSHI U, ATSUSHI N. Orbital maintenance of super low altitude satellite by new frozen orbit. Proc. of the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration, 2008: 23−31.
15	ZHANG J, LI H Y, LUO Y Z, et al. Effects of in-track maneuver on the ground track of near-circular orbits. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1373−1378.
16	THOMAS C C, COSTANTINOS Z, JONATHAN T B Responsive satellites through ground track manipulation using existing technology. Journal of Spacecraft and Rockets, 2013, 50 (1): 220- 229.
17	THOMAS C C, JONATHAN T B Responsiveness in low orbits using electric propulsion. Journal of Spacecraft and Rockets, 2014, 51 (3): 938- 945. doi: 10.2514/1.A32405
18	ZHANG H Y, ZHANG G Reachable domain of ground track with a single impulse. IEEE Trans. on Aerospace and Electronic Systems, 2021, 57 (2): 1105- 1122.
19	SHENG J, ZHANG G, GENG Y H. Analytical method for ground track manipulation using impulse thrust based on J2 perturbation. Journal of Astronautic, 2016, 37(8): 21−27.
20	LIN X, ZHANG G, ZHANG H Y. Multi-target ground-track adjustment with a single coplanar impulse. Aerospace Science and Technology, 2021, 119: 107135.
21	FU X F, WU M P, TANG Y Design and maintenance of low-Earth repeat-ground-track successive-coverage orbits. Journal of Guidance, Control, and Dynamics, 2012, 35 (2): 686- 691. doi: 10.2514/1.54780
22	SALAMA O. Autonomous orbit maintenance law for LEO sun synchronous, earth repeating satellites with electric propulsion system. Proc. of the AIAA/AAS Astrodynamics Specialist Conference and Exhibit, 2008. DOI: 10.2514/6.2008-7197.
23	CO T C, ZAGARIS C, BLACK J T Responsive satellites through ground track manipulation using existing technology. Journal of Spacecraft and Rockets, 2013, 50 (1): 206- 216. doi: 10.2514/1.A32263

Adjustment of the number of days/day	Change in tangent velocity/ (m·s⁻¹)	Minimum distance to the target point/km	Distance to target point without manipulation/km
3	−20.62	28.4	942.4
4	−15.04	28.8	920.0
5	−11.60	27.6	891.0
6	−9.23	27.4	855.5

Method of SLAS’s ground track manipulation based on tangential impulse thrust

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