通导一体化环月星座设计初探

doi:10.12305/j.issn.1001-506X.2023.01.28

Abstract

Abstract:

With the further development of lunar exploration activities, the requirements for continuity of coverage, immediacy of communication, precision of navigation and construction cost of lunar relay constellation are becoming higher and higher. The integration of communication and navigation can bring new ideas to the design of lunar constellations. In addition to providing communication relay services for lunar users, it can also achieve high-precision positioning for them under triple coverage. For the lunar orbit constellations with different number of satellites and different orbit heights, the performance of their coverage continuities for single, double and triple coverage is analyzed, and the theoretical minimum number of satellites required for different coverage multiples at a specific altitude is proposed and simulations are performed to verify. Then, with the design criterion of integration of communication and navigation, the simulation of the lunar users positioning under triple coverage is carried out, and the results show that the positioning accuracy of triple coverage can reach meter level.

Key words: constellation orbiting the moon, communication and navigation integration, coverage performance, positioning accuracy

CLC Number:

Xiaowei WANG, Yafeng ZHAN, Haoran XIE, Xi CHEN. A preliminary study on the design of constellation orbiting the moon with the communication and navigation integration[J]. Systems Engineering and Electronics, 2023, 45(1): 241-249.

Figures/Tables 20

Fig.1

Fig.2

Fig.3

Table 1

Fig.4

Fig.5

Fig.6

Fig.7

Table 2

Fig.8

Fig.9

Table 3

Fig.10

Fig.11

Fig.12

Fig.13

Fig.14

Table 4

Fig.15

Fig.16

References 40

1	International Space Exploration Coordination Group . Global exploration roadmap[M]. Washington: National Aeronautics and Space Administration Headquarters, 2018.
2	SMITH M, CRAIG D, HERRMANN N, et al. The artemis program: an overview of NASA's activities to return humans to the moon[C]//Proc. of the IEEE Aerospace Conference, 2020.
3	PRABU T , MUTHUKKUMARAN K , VENUGOPAL I . Assessment of dynamic properties of a new lunar highland soil simulant (LSS-ISAC-1) developed for Chandrayaan missions[J]. Soil Dynamics and Earthquake Engineering, 2022, 155, 107- 178.
4	张扬眉. 2019年国外空间探测发展综述[J]. 国际太空, 2020, 2, 24- 29.
	ZHANG Y M . A review of foreign space exploration development in 2019[J]. Space International, 2020, 2, 24- 29.
5	State Council Information Office of the People's Republic of China. China's space program: a 2021 perspective[EB/OL]. [2022-02-11]. https://english.news.cn/20220128/6b7a3f-42392949778b334ae12a8c93c9/c.html.
6	王猛, 刘蕾, 汤丁诚, 等. 月球航天器GNSS自主导航可行性分析及设计[C]//中国卫星导航学术年会, 2017.
	WANG M, LIU L, TANG D C, et al. Feasibility analysis and design of GNSS autonomous navigation for Lunar Spacecraft[C]//Proc. of the China Satellite Navigation Annual Conference, 2017.
7	CAPUANO V . GNSS-based navigation for lunar missions[M]. Lausanne: école Polytechnique Fédérale de Lausanne, 2016.
8	STANLEY D, COOK S, CONNOLLY J, et al. NASA's exploration systems architecture study-final report[R]. New York: AIAA Space Systems Technical Committee, 2005: 1-58.
9	FOUST J . Moon base: the next step in the exploration of the solar system[J]. Ad Astra, 2007, 19 (2): 28- 31.
10	Space Communication Architecture Working Group. NASA space communication and navigation architecture recommendations for 2005-2030[R]. Washington: National Aeronautics and Space Administration, 2006.
11	孙超. 月球探测星座构型与部署轨道设计方法研究[D]. 北京: 北京理工大学, 2018.
	SUN C. Research on configuration and deployment orbit design of lunar exploration constellation[D]. Beijing: Beijing Institute of Technology, 2018.
12	SELENE Project Team. Scientific research in SELENE mission[R]. Tokyo: Institute of Space and Astronautical Sciences of Japan, 2000.
13	RISE Lunar Orbiter Developing Group. The designation report on RISE mission concept[R]. Tokyo: National Astronomical Observatorty of Japan, 1999.
14	刘磊, 胡松杰, 唐歌实, 等. 月球中继通信与导航的研究进展与建议[C]//中国宇航学会深空探测技术专业委员会第十届学术年会论文集, 2013: 439-444.
	LIU L, HU S J, TANG G S, et al. Research progress and suggestions on lunar relay communication and navigation[C]//Proc. of the 10th Annual Conference of Deep Space Exploration Technology Committee, 2013: 439-444.
15	ILK K H . Satellite-to-satellite-tracking[M]. Berlin: Springer Spektrum, 2021: 215- 231.
16	CHEN Y X , ZHANG J , LIU X . Application of GPS in satellite to satellite tracking (SST) technology[J]. Fire Control Radar Technology, 2017, 46 (2): 15- 21, 26. doi: 10.3969/j.issn.1008-8652.2017.02.003
17	PARKER J S, ANDERSON R L, BORN G H, et al. Linked autonomous interplanetary satellite orbit navigation[R]. Washington: NASA Tech Briefs, 2013: 32-33.
18	HESAR S G , PARKER J S , LEONARD J M , et al. Lunar far side surface navigation using linked autonomous interplanetary satellite orbit navigation (LiAISON)[J]. Acta Astronautica, 2015, 117, 116- 129. doi: 10.1016/j.actaastro.2015.07.027
19	PARKER J S, ANDERSON R L. Navigation between geosynchronous and lunar L1 orbiters[C]//Proc. of the AIAA/AAS Astrodynamics Specialist Conference, 2012.
20	FUJIMOTO K, LEONARD J M, MCGRANAGHAN R M, et al. Simulating the LiAISON navigation concept in a GEO + Earth-Moon halo constellation[C]//Proc. of the 23rd International Symposium on Space Flight Dynamics, 2012.
21	LIU B, HOU X Y, TANG J S, et al. Autonomos orbit determination of satellites around triangular libration points in the Earth-Moon system[C]//Proc. of the 28th Conference of Spacecraft TT&C Technology, 2016: 371-384.
22	ZHANG L , XU B . Navigation performance of the libration point satellite navigation system in cislunar space[J]. Journal of Navigation, 2015, 68 (2): 367- 382. doi: 10.1017/S0373463314000617
23	WOODARD M, FOLTA D, WOODFORK D. ARTEMIS: the first mission to the lunar libration orbits[C]//Proc. of the 21st International Symposium on Space Flight Dynamics, 2009.
24	ANGELOPOULOS V . The artemis mission[M]. Berlin: Springer, 2010: 3- 25.
25	YI Q , ANTON D R . Transfers to lunar libration point orbits[J]. Communications in Nonlinear Science and Numerical Simulation, 2019, 74, 180- 200. doi: 10.1016/j.cnsns.2019.01.033
26	FOLTA D C , WOODARD M , HOWELL K , et al. Applications of multi-body dynamical environments: the ARTEMIS transfer trajectory design[J]. Acta Astronautica, 2012, 73, 237- 249. doi: 10.1016/j.actaastro.2011.11.007
27	LIU L , LI J S . CHANG'E-5T1 extended mission: the first lunar libration point flight via a lunar swing-by[J]. Advances in Space Research, 2016, 58, 609- 618. doi: 10.1016/j.asr.2016.05.015
28	DUAN J F , WANG Z K . Orbit determination of CE-4's relay satellite in Earth-Moon L2 libration point orbit[J]. Advances in Space Research, 2019, 64 (11): 2345- 2355. doi: 10.1016/j.asr.2019.08.012
29	PAN S S , HOU X Y . Two-maneuver transfers from the collinear L2 point to the triangular L4 point in the planar Earth-Moon system[J]. Advances in Space Research, 2020, 65 (12): 2878- 2893. doi: 10.1016/j.asr.2020.03.022
30	NOREEN G K . An integrated mobile satellite broadcast, paging, communications and navigation system[J]. IEEE Trans.on Broadcasting, 1990, 36 (4): 270- 274. doi: 10.1109/11.64477
31	AI G X , SHI H L , WU H T , et al. The principle of the positioning system based on communication satellites[J]. Science in China, 2009, 52 (3): 472- 488.
32	KAIVANTO E K , BERG M , SALONEN E , et al. Wearable circularly polarized antenna for personal satellite communication and navigation[J]. IEEE Trans.on Antenna and Propagation, 2011, 59 (12): 4490- 4496. doi: 10.1109/TAP.2011.2165513
33	蔚保国, 鲍亚川, 杨梦焕, 等. 通导一体化概念框架与关键技术研究进展[J]. 导航定位与授时, 2022, 9 (2): 1- 14.
	YU B G , BAO Y C , YANG M H , et al. Research progress on conceptual framework and key technologies of communication and navigation integration[J]. Navigation, positioning and timing, 2022, 9 (2): 1- 14.
34	LI X Y, YAN Y J, ZOU D Y. A master-slave rake receiver for integrated navigation/communication signal[C]//Proc. of the International Wireless Communications and Mobile Computing, 2021: 1070-1074.
35	ZOU D Y , LI X Y , MA R F . A signal optimization strategy for next generation navigation and communication integration applications[J]. Physical Communication, 2022, 50, 101510. doi: 10.1016/j.phycom.2021.101510
36	LI R , ZHENG S Y , WANG E S , et al. Advances in BeiDou navigation satellite system(BDS)and satellite navigation augmentation technologies[J]. Satellite Navigation, 2020, 1, 12. doi: 10.1186/s43020-020-00010-2
37	LI G , GUO S R , LV J , et al. Introduction to global short message communication service of BeiDou-3 navigation satellite system[J]. Advances in Space Research, 2021, 67 (5): 1701- 1708. doi: 10.1016/j.asr.2020.12.011
38	YANG Y X , GAO W G , GUO S R , et al. Introduction to BeiDou-3 navigation satellite system[J]. Navigation, 2019, 66 (1): 7- 18. doi: 10.1002/navi.291
39	CUI J X , SHI H L , CHEN J B , et al. The transmission link of CAPS navigation and communication system[J]. Science in China, 2009, 52 (3): 402- 411. doi: 10.1007/s11430-009-0034-y
40	谢浩然, 詹亚锋, 王晓伟, 等. 卫星通导一体化技术及其在探月中的应用[J]. 深空探测学报, 2021, 8 (2): 154- 162.
	XIE H R , ZHAN Y F , WANG X W , et al. Satellite communication and navigation integration technology and its application in lunar exploration[J]. Journal of Deep Space Exploration, 2021, 8 (2): 154- 162.

轨道根数	取值
偏心率e	0
倾角i/(°)	60
近月点幅角ω/(°)	0
升交点赤经Ω/(°)	0, 72, 144, 216, 288
真近点角f/(°)	0, 72, 144, 216, 288

轨道根数	取值
偏心率e	0
倾角i/(°)	60
近月点幅角ω/(°)	0
升交点赤经Ω/(°)	0, 45, 90, 135, 180, 225, 270, 315
真近点角f/(°)	0, 45, 90, 135, 180, 225, 270, 315

轨道根数	取值
偏心率e	0
倾角i/(°)	60
近月点幅角ω/(°)	0
升交点赤经Ω/(°)	0, 0, 0, 0, 120, 120, 120, 120, 240, 240, 240, 240
真近点角f/(°)	0, 90, 180, 270, 30, 120, 210, 300, 60, 150, 240, 330

坐标点	纬度/(°)	经度/(°)
1	42	237
2	63	87
3	-48	312
4	-63	27

[1]	XU Zhaoxin, LI Hangzhou, LI Liang, ZHAO Lin, LIU Ya. EKF/SF-based short-baseline BDS multipath mitigation method [J]. Systems Engineering and Electronics, 2017, 39(6): 1334-1340.
[2]	ZHAO Lin, ZHANG Sheng-zong, LI Liang, WANG Xue. BDS/GPS integrated precise point positioning based on adaptive extended Kalman filter [J]. Systems Engineering and Electronics, 2016, 38(9): 2142-2148.

A preliminary study on the design of constellation orbiting the moon with the communication and navigation integration

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 20

References 40

Related Articles 2

Recommended Articles

Metrics

Comments