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PROCYON Mission Reanalysis: Low-Thrust Asteroid Flyby Trajectory Design leveraging Convex Programming PROCYON任务再分析：利用凸规划的低推力小行星飞越轨道设计
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-02-01 DOI: 10.1007/s40295-021-00299-4
N. Ozaki, K. Oguri, R. Funase
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引用次数: 1
Motivation and Concept for Improved Laboratory Simulation of Space Electron Fluxes 改进空间电子通量实验室模拟的动机和概念
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-02-01 DOI: 10.1007/s40295-021-00298-5
M. Bengtson, C. Hooper, R. Hoffmann, D. Engelhart, Vanessa J. Murray, D. Ferguson
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引用次数: 0
Bayesian Approach to Light Curve Inversion of 2020 SO 2020年SO光曲线反演的贝叶斯方法
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-02-01 DOI: 10.1007/s40295-021-00301-z
T. Campbell, R. Furfaro, V. Reddy, Adam Battle, P. Birtwhistle, T. Linder, S. Tucker, N. Pearson
{"title":"Bayesian Approach to Light Curve Inversion of 2020 SO","authors":"T. Campbell, R. Furfaro, V. Reddy, Adam Battle, P. Birtwhistle, T. Linder, S. Tucker, N. Pearson","doi":"10.1007/s40295-021-00301-z","DOIUrl":"https://doi.org/10.1007/s40295-021-00301-z","url":null,"abstract":"","PeriodicalId":50009,"journal":{"name":"Journal of the Astronautical Sciences","volume":null,"pages":null},"PeriodicalIF":1.8,"publicationDate":"2022-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"42622609","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
Spectral Characteristics of GEO Satellite Arcing – 300 To 350 MHz 地球同步轨道卫星电弧的频谱特性–300至350 MHz
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-25 DOI: 10.1007/s40295-021-00295-8
D. Ferguson, P. Perillat, B. Vayner
{"title":"Spectral Characteristics of GEO Satellite Arcing – 300 To 350 MHz","authors":"D. Ferguson, P. Perillat, B. Vayner","doi":"10.1007/s40295-021-00295-8","DOIUrl":"https://doi.org/10.1007/s40295-021-00295-8","url":null,"abstract":"","PeriodicalId":50009,"journal":{"name":"Journal of the Astronautical Sciences","volume":null,"pages":null},"PeriodicalIF":1.8,"publicationDate":"2022-01-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"45614719","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Closed Loop Guidance During Close Range Rendezvous in a Three Body Problem 三体问题中近距离交会过程中的闭环制导
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-23 DOI: 10.1007/s40295-021-00289-6
Michele Galullo, Giordana Bucchioni, G. Franzini, M. Innocenti
{"title":"Closed Loop Guidance During Close Range Rendezvous in a Three Body Problem","authors":"Michele Galullo, Giordana Bucchioni, G. Franzini, M. Innocenti","doi":"10.1007/s40295-021-00289-6","DOIUrl":"https://doi.org/10.1007/s40295-021-00289-6","url":null,"abstract":"","PeriodicalId":50009,"journal":{"name":"Journal of the Astronautical Sciences","volume":null,"pages":null},"PeriodicalIF":1.8,"publicationDate":"2022-01-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"43817498","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 6
Effects of Tow Parameters on Dynamic Behaviors of Beam-type Orbital Debris 拖曳参数对波束型轨道碎片动力学特性的影响
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-18 DOI: 10.1007/s40295-021-00297-6
Weipeng Hu, Yulu Huai, Mengbo Xu, Peixin Cao, Ruisong Jiang, J. Shi, Z. Deng
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引用次数: 3
Identifying Radiation Induced Spectroscopic Changes in Polyimide Materials 识别聚酰亚胺材料中辐射诱导的光谱变化
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-17 DOI: 10.1007/s40295-021-00291-y
D. Engelhart, J. Reyes, Vanessa G. Murray, D. Ferguson, R. Hoffmann
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引用次数: 2
“Comments on a Paper of Idrisi, Ullah and Sikkandhar (Effect of Perturbations in Coriolis and Centrifugal Forces on Libration Points in the Restricted Six-Body Problem: JAS (2021) 68:4-25)” 对Idrisi, Ullah和Sikkandhar的一篇论文的评论(限制六体问题中科里奥利力和离心力扰动对振动点的影响:JAS (2021) 68:4-25)
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-15 DOI: 10.1007/s40295-021-00294-9
A. Elipe
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引用次数: 0
Low-Thrust Lunar Capture Leveraging Nonlinear Orbit Control 利用非线性轨道控制的低推力月球捕获
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-03 DOI: 10.1007/s40295-023-00391-x
M. Pontani, M. Pustorino
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引用次数: 1
A Homotopic Direct Collocation Approach for Operational-Compliant Trajectory Design. 一种操作柔性轨迹设计的同伦直接搭配方法。
IF 1.8 4区 工程技术 Q3 Engineering
Journal of the Astronautical Sciences
Pub Date : 2022-01-01 DOI: 10.1007/s40295-022-00351-x
Alessandra Mannocchi, Carmine Giordano, Francesco Topputo

Stand-alone deep-space CubeSats are the future of the space sector. For limited budget reasons, these spacecraft need to follow operational-compliant (OC) trajectories: transfers with thrusting and coasting periods imposed at pre-defined time instants. Traditional trajectory optimisation algorithms exhibit convergence problems when handling discontinuous constraints. In this work, a homotopic direct collocation approach is presented. It employs a continuation algorithm that maps the classical bang-bang trajectory of a fuel-optimal low-thrust problem into an OC solution. M-ARGO CubeSat mission is considered as case study for validation, including a realistic thruster model with variable specific impulse and maximum thrust. The trajectories computed with the developed algorithm are compared with non-operational-compliant solutions. Our algorithm produces transfers similar to the optimal solutions with no operational constraint, both in terms of thrusting profile and propellant mass.

独立的深空立方体卫星是太空领域的未来。由于预算有限，这些航天器需要遵循操作兼容(OC)轨迹:在预先定义的时间瞬间施加推力和滑行周期的转移。传统的轨迹优化算法在处理不连续约束时存在收敛性问题。本文提出了一种同伦直接搭配方法。它采用了一种延拓算法，将燃料最优低推力问题的经典砰砰轨迹映射到OC解中。M-ARGO立方体卫星任务作为验证的案例研究，包括一个具有可变比冲和最大推力的现实推进器模型。用该算法计算的轨迹与非操作兼容解进行了比较。我们的算法产生的传输与最优解相似，没有操作约束，无论是在推力剖面还是推进剂质量方面。
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引用次数: 0
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