多地球同步航天器换料的多目标任务规划

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE International Journal of Aerospace Engineering Pub Date : 2023-09-06 DOI:10.1155/2023/6623461
Linjie Kong, Yang Zhou
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引用次数: 0

摘要

研究了具有多个服务航天器和多个燃料库的多地球同步航天器加注问题。在任务场景中,多个Ssc和fd最初停放在地球同步轨道(GEO)上。Ssc从FDs和机动开始访问并为已知需求的多个GEO目标加油。这些有能力的Ssc预计将与燃料不足的GEO目标和fd会合,以便将储存在fd中的燃料输送到GEO目标。目标是找到一组具有最小燃料成本和任务持续时间的帕累托最优解。MGSRP是混合离散变量和连续变量的多仓库车辆路线问题的更复杂的变体。建立了双嵌套优化模型。提出了一种新的多目标混合粒子群优化方法来解决外环问题,设计变量为加油顺序、任务分配、时间分布和fd位置。在内环问题中,采用分支定界法寻找给定外环解的最优决策变量。最后,通过数值仿真验证了所提方法的有效性。
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Multiobjective Mission Planning for Multiple Geosynchronous Spacecraft Refueling
This paper studies the multiple geosynchronous spacecraft refueling problem (MGSRP) with multiple servicing spacecraft (Ssc) and fuel depots (FDs). In the mission scenario, multiple Ssc and FDs are parked in the geosynchronous Earth orbit (GEO) initially. Ssc start from FDs and maneuver to visit and refuel multiple GEO targets with known demands. These capacitated Ssc are expected to rendezvous with fuel-deficient GEO targets and FDs for the purpose of delivering the fuel stored in FDs to GEO targets. The objective is to find a set of Pareto-optimal solutions with minimum fuel cost and mission duration. The MGSRP is a much more complex variant of multidepot vehicle routing problems mixing discrete and continuous variables. A two-nested optimization model is built. We propose a new multiobjective hybrid particle swarm optimization to solve the outer-loop problem, and the design variables are the refueling sequence, task assignment, time distribution, and locations of FDs. In the inner-loop problem, branch and bound method is used to find the optimal decision variable for a given outer-loop solution. Finally, numerical simulations are presented to illustrate the effectiveness and validity of the proposed approach.
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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