TY - JOUR
T1 - 基于METRIC理论的超大规模卫星星座多级备份策略
AU - Luo, Tiansu
AU - Zhao, Lingfeng
AU - Feng, Yunwen
AU - Xue, Xiaofeng
AU - Lu, Cheng
N1 - Publisher Copyright:
© 2022, Editorial Office of Systems Engineering and Electronics. All right reserved.
PY - 2022/7/1
Y1 - 2022/7/1
N2 - Aiming at the possible problems of high operation and maintenance cost and low mission availability of super large-scale satellite constellation, combined with the current situation of mass production of satellites and the use of one rocket to put multiple satellites into orbit (one rocket with multiple satellites), a multi-level backup strategy of super large-scale satellite constellation is proposed based on the optimization method of multi-echelon technology for recoverable item control (METRIC). Firstly, the principle of the multi-stage backup strategy model of a satellite constellation based on METRIC theory is explained. The backup strategy considers three backup modes: ground backup, parking orbit backup, and constellation orbit backup. The constellation availability model considers the satellites' average annual demand number, expected demand number, and expected shortage number. The constellation backup cost model includes manufacturing cost and launch cost, and the mathematical optimization model with constellation availability as the constraint and constellation annual backup cost as the optimization objective. Then, a case study of a super large-scale constellation is developed and solved by using both genetic algorithm and marginal analysis. Finally, the advantages and disadvantages of the genetic algorithm and marginal analysis in solving this optimization problem are discussed. Result shows that the model significantly reduces the backup cost of a large-scale satellite constellation while ensuring the constellation availability, and provides guidance for the accurate allocation of the number of backup satellites at each level.
AB - Aiming at the possible problems of high operation and maintenance cost and low mission availability of super large-scale satellite constellation, combined with the current situation of mass production of satellites and the use of one rocket to put multiple satellites into orbit (one rocket with multiple satellites), a multi-level backup strategy of super large-scale satellite constellation is proposed based on the optimization method of multi-echelon technology for recoverable item control (METRIC). Firstly, the principle of the multi-stage backup strategy model of a satellite constellation based on METRIC theory is explained. The backup strategy considers three backup modes: ground backup, parking orbit backup, and constellation orbit backup. The constellation availability model considers the satellites' average annual demand number, expected demand number, and expected shortage number. The constellation backup cost model includes manufacturing cost and launch cost, and the mathematical optimization model with constellation availability as the constraint and constellation annual backup cost as the optimization objective. Then, a case study of a super large-scale constellation is developed and solved by using both genetic algorithm and marginal analysis. Finally, the advantages and disadvantages of the genetic algorithm and marginal analysis in solving this optimization problem are discussed. Result shows that the model significantly reduces the backup cost of a large-scale satellite constellation while ensuring the constellation availability, and provides guidance for the accurate allocation of the number of backup satellites at each level.
KW - Backup strategy
KW - Genetic algorithm (GA)
KW - Multi-echelon technique for recoverable item control (METRIC) theory
KW - Satellite constellation
UR - http://www.scopus.com/inward/record.url?scp=85132539463&partnerID=8YFLogxK
U2 - 10.12305/j.issn.1001-506X.2022.07.14
DO - 10.12305/j.issn.1001-506X.2022.07.14
M3 - 文章
AN - SCOPUS:85132539463
SN - 1001-506X
VL - 44
SP - 2181
EP - 2190
JO - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
JF - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
IS - 7
ER -