Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing

With the rapid development of on-orbit services and space situational awareness, there is an urgent demand for multisatellite flyby inspection (MSFI) that can obtain information about a large number of space targets with little fuel consumption in a short time. There are two kinds of constraints, na...

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Main Authors: Chenyuan Peng, Jin Zhang, Bing Yan, Yazhong Luo
Format: Article
Language:English
Published: MDPI AG 2021-09-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/8/9/274
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spelling doaj-f8b0b47f67f2420c9aca802beef12b3e2021-09-25T23:33:23ZengMDPI AGAerospace2226-43102021-09-01827427410.3390/aerospace8090274Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint RepairingChenyuan Peng0Jin Zhang1Bing Yan2Yazhong Luo3College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, ChinaCollege of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, ChinaWith the rapid development of on-orbit services and space situational awareness, there is an urgent demand for multisatellite flyby inspection (MSFI) that can obtain information about a large number of space targets with little fuel consumption in a short time. There are two kinds of constraints, namely inspection constraints (ICs) at each flyby point and transfer process constraints (TPCs) in the actual mission. Further considering the influence of discrete and continuous variables such as inspection sequence, time, and maneuver scheme, it is complex and difficult to solve MSFI. To optimize it efficiently, the task flow and the problem model are defined firstly. Then, the algorithm framework based on constraint repairing is given, which contains repair methods of the ICs and the TPCs. Finally, the proposed method is compared with the nonrepair optimization method in two numerical examples. The results indicate that when the constraints are hard to meet, it is better and more efficient than the nonrepair method.https://www.mdpi.com/2226-4310/8/9/274multisatellite flyby inspectionconstraint repairingtrajectory optimizationon-orbit servicesspace situational awareness
collection DOAJ
language English
format Article
sources DOAJ
author Chenyuan Peng
Jin Zhang
Bing Yan
Yazhong Luo
spellingShingle Chenyuan Peng
Jin Zhang
Bing Yan
Yazhong Luo
Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing
Aerospace
multisatellite flyby inspection
constraint repairing
trajectory optimization
on-orbit services
space situational awareness
author_facet Chenyuan Peng
Jin Zhang
Bing Yan
Yazhong Luo
author_sort Chenyuan Peng
title Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing
title_short Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing
title_full Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing
title_fullStr Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing
title_full_unstemmed Multisatellite Flyby Inspection Trajectory Optimization Based on Constraint Repairing
title_sort multisatellite flyby inspection trajectory optimization based on constraint repairing
publisher MDPI AG
series Aerospace
issn 2226-4310
publishDate 2021-09-01
description With the rapid development of on-orbit services and space situational awareness, there is an urgent demand for multisatellite flyby inspection (MSFI) that can obtain information about a large number of space targets with little fuel consumption in a short time. There are two kinds of constraints, namely inspection constraints (ICs) at each flyby point and transfer process constraints (TPCs) in the actual mission. Further considering the influence of discrete and continuous variables such as inspection sequence, time, and maneuver scheme, it is complex and difficult to solve MSFI. To optimize it efficiently, the task flow and the problem model are defined firstly. Then, the algorithm framework based on constraint repairing is given, which contains repair methods of the ICs and the TPCs. Finally, the proposed method is compared with the nonrepair optimization method in two numerical examples. The results indicate that when the constraints are hard to meet, it is better and more efficient than the nonrepair method.
topic multisatellite flyby inspection
constraint repairing
trajectory optimization
on-orbit services
space situational awareness
url https://www.mdpi.com/2226-4310/8/9/274
work_keys_str_mv AT chenyuanpeng multisatelliteflybyinspectiontrajectoryoptimizationbasedonconstraintrepairing
AT jinzhang multisatelliteflybyinspectiontrajectoryoptimizationbasedonconstraintrepairing
AT bingyan multisatelliteflybyinspectiontrajectoryoptimizationbasedonconstraintrepairing
AT yazhongluo multisatelliteflybyinspectiontrajectoryoptimizationbasedonconstraintrepairing
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