Journal of Systems Engineering and Electronics ›› 2023, Vol. 34 ›› Issue (5): 1267-1284.doi: 10.23919/JSEE.2023.000067
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收稿日期:2022-07-12出版日期:2023-10-18发布日期:2023-10-30
Research on agile space emergency launching mission planning simulation and verification method
Feng WU1,*(
), Xiuluo LIU1(), Jia WANG1(), Chao LI2(), Ying LIU1(), Jianbin SU1(), Ailiang ZHANG1(), Min WANG1()
- 1 Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China
2 CASIC Space Engineering Development Co. Ltd., Beijing 100854, China
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Received:2022-07-12Online:2023-10-18Published:2023-10-30 -
Contact:Feng WU E-mail:2904099828@qq.com;glenliu@263.net;kelexuebi2009@163.com;446591391@qq.com;fq_1982@126.com;sujianbin1983@163.com;zhangailiang1966@126.com;2548181884@qq.com -
About author:
WU Feng was born in 1980. He received his bachelor ’s degree in applied mathematics from the Department of Mathematics, Huazhong University of Science and Technology, Wuhan, China in 2003. He received his master’s degree in applied mathematics from the Department of Mathematics in National University of Defense Technology, Changsha, China in 2005. He received his Ph.D. degree in computer science and technology from the Computer College in National University of Defense Technology, Changsha, China in 2009. From January 2010 to now, he is an assistant research fellow with Beijing Institute of Tracking and Telecommunications Technology and his main research direction is space launching informatization. His research interests include distributed computing software, computer simulation, scientific computation, and data visualization. E-mail: 2904099828@qq.com
LIU Xiuluo was born in 1974. He received his B.E., and Ph.D. degrees in control science and engineering from National University of Defense Technology, Changsha, China, in 1996, and 2001, respectively. From December 2002 to December 2004, he held a Postdoctoral Fellowship in the Training Simulation Center, National Defense University. He is currently an associate research fellow with Beijing Institute of Tracking and Telecommunications Technology. His research interests include system simulation and digital engineering in aerospace. E-mail: glenliu@263.net
WANG Jia was born in 1983. She received her B.E., and M.E. degrees in computer science and technology from National University of Defense Technology, Changsha, China, in 2004 and 2006, respectively. She is currently an assistant research fellow with Beijing Institute of Tracking and Telecommunications Technology. Her research interests include launch informatization and test evaluation. E-mail: kelexuebi2009@163.com
LI Chao was born in 1990. He received his Ph.D. degree in control science and engineering from the Department of Automation, Beijing Institute of Technology, Beijing, China, in 2019. He works as an intermediate engineer at CASIC Space Engineering Development Co. Ltd., Beijing, China. His research interest is space launching informatization. E-mail: 446591391@qq.com
LIU Ying was born in 1979. He received his bachelor’s degree from East China Jiaotong University in 2001 and master ’s degree from Beihang University in 2004. From April 2004 to now, he is an associate research fellow with Beijing Institute of Tracking and Telecommunications Technology. His research interests include carrier rocket entire design, test and launching. E-mail: fq_1982@126.com
SU Jianbin was born in 1983. He received his B.E., M.E., and Ph.D. degrees in control science and engineering from National University of Defense Technology, Changsha, China, in 2006, 2008, and 2013, respectively. He is currently an assistant research fellow with Beijing Institute of Tracking and Telecommunications Technology. His research interest is rapid launch in aerospace. E-mail: sujianbin1983@163.com
ZHANG Ailiang was born in 1966. In 1990 and 2014, he received his bachelor ’s degree from Wuhan University of Surveying and Mapping Technology and master ’s degree in engineering from Beijing Institute of Technology. He has been engaged in command and control of space launching and is now an associate researcher with Beijing Institute of Tracking and Telecommunications Technology. His research interests include space launch informatization and test evaluation. E-mail: zhangailiang1966@126.com
WANG Min was born in 1990. He received his B.E. degree from Chengdu University of Technology, Chengdu, China, in 2015. He is currently an assistant research fellow with Beijing Institute of Tracking and Telecommunications Technology. His research interest is space launching digitization. E-mail: 2548181884@qq.com
引用本文
. [J]. Journal of Systems Engineering and Electronics, 2023, 34(5): 1267-1284.
Feng WU, Xiuluo LIU, Jia WANG, Chao LI, Ying LIU, Jianbin SU, Ailiang ZHANG, Min WANG. Research on agile space emergency launching mission planning simulation and verification method[J]. Journal of Systems Engineering and Electronics, 2023, 34(5): 1267-1284.
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| Orbital height/km | SSO | LEO | Retrograde orbit | Summation | |||||||||||
| T-Q | S-Q | S-R/% | T-Q | S-Q | S-R/% | T-Q | S-Q | S-R/% | T-Q | S-Q | S-R/% | ||||
| 268 | 0 | 0 | - | 0 | 0 | - | 54 | 49 | 90.74 | 54 | 49 | 90.74 | |||
| 286 | 0 | 0 | - | 0 | 0 | - | 52 | 43 | 82.69 | 52 | 43 | 82.69 | |||
| 300 | 52 | 49 | 94.23 | 48 | 43 | 89.58 | 52 | 45 | 86.54 | 152 | 137 | 90.13 | |||
| 400 | 0 | 0 | - | 24 | 24 | 100 | 0 | 0 | - | 24 | 24 | 100 | |||
| 500 | 52 | 50 | 96.15 | 48 | 46 | 95.83 | 0 | 0 | - | 100 | 96 | 96 | |||
| 700 | 52 | 49 | 94.23 | 24 | 23 | 95.83 | 0 | 0 | - | 76 | 72 | 94.74 | |||
| Summation | 156 | 148 | 94.87 | 144 | 136 | 94.44 | 158 | 137 | 86.71 | 458 | 421 | 91.92 | |||
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| Orbital height/km | SSO/% | LEO/% | Retrograde orbit/% |
| 268 | 0 | 0 | 13.51 |
| 286 | 0 | 0 | 24.32 |
| 300 | 8.11 | 13.51 | 18.92 |
| 400 | 0 | 0 | 0 |
| 500 | 5.41 | 5.41 | 0 |
| 700 | 8.11 | 2.70 | 0 |
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| Orbit parameter | Number |
| Orbit semi-major axis/km | 6646.137 |
| Trajectory inclination/(°) | 139 |
| Orbital eccentricity | 0 |
| Orbital plane number | 4 |
| Satellite number in each orbital plane | 6 |
| Phase factor | 1 |
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| Satellite | Launching time window (UTC time) | ||
| Launching area 1 | Launching area 2 | Launching area 3 | |
| The first orbital plane No.1-3 satellite | March 18, 2022 22:23:58.575−22:24:20.931 | —— | —— |
| The first orbital plane No.4-6 satellite | —— | March 18, 2022 00:32:55.090−00:32:57.466 | —— |
| The second orbital plane No.1-3 satellite | March 18, 2022 04:22:03.49−04:22:23.732 | —— | —— |
| The second orbital plane No.4-6 satellite | —— | March 18, 2022 06:28:44.850−06:28:55.940 | —— |
| The third orbital plane No.1-3 satellite | March 18, 2022 11:43:38.056−11:44:16.717 | —— | —— |
| The third orbital plane No.4-6 satellite | —— | March 18, 2022 12:24:38.860−12:24:50.151 | —— |
| The fourth orbital plane No.1-3 satellite | March 18, 2022 17:39:29.764−17:40:08.737 | —— | —— |
| The fourth orbital plane No.4-6 satellite | —— | —— | March 18, 2022 14:05:58.264−14:06:15.460 |
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| Latitude coordinate/(°) | Average revisit time (hour, minute, second) | The max revisit time (hour, minute, second) |
| 25.05 | 0:56:38 | 4:01:47 |
| 24.1386 | 1:07:31 | 3:47:47 |
| 23.1725 | 1:07:31 | 3:33:49 |
| 22.6306 | 0:58:01 | 3:33:49 |
| 22.6667 | 1:04:26 | 3:33:50 |
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