Verification of Tether Deployment System aboard CubeSat through Dynamics Simulations and Tests

被引：4

作者：

Sakamoto, Hiraku ^{[1
]}

Mughal, Muhammad Rizwan ^{[2
]}

Slavinskis, Andris ^{[2
]}

Praks, Jaan ^{[2
]}

Toivanen, Petri ^{[3
]}

Janhunen, Pekka ^{[3
]}

Palmroth, Minna ^{[4
]}

Kilpua, Emilia ^{[4
]}

Vainio, Rami ^{[5
]}

机构：

[1] Tokyo Inst Technol, Meguro Ku, 2-12-1 Ookayama, Tokyo 1528552, Japan

[2] Aalto Univ, Maarintie 8, Espoo 02150, Finland

[3] Finnish Meteorol Inst, POB 503, FI-00101 Helsinki, Finland

[4] Univ Helsinki, POB 68, FI-00014 Helsinki, Finland

[5] Univ Turku, Dept Phys & Astron, Turku 20014, Finland

来源：

2021 IEEE AEROSPACE CONFERENCE (AEROCONF 2021) | 2021年

基金：

芬兰科学院;

关键词：

WIRE;

D O I：

10.1109/AERO50100.2021.9438281

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper proposes a proper model selection strategies for the dynamic simulations of the tether deployment mission aboard a CubeSat. Space tether technology will enable innovative space missions in the near future. The Coulomb Drag Propulsion (CDP), including electric solar wind sailing, is one of the plausible future technologies. The authors currently develop a CubeSat, FORESAIL-1, for space demonstration of CDP. However, the analytical simulations for the verification and validation of the mission design typically require a high computational cost. This is because a minimum model order is not selected properly. In this study, through observing a preliminary analytical model for tether deployment analysis, the simplest model is chosen to avoid the mission failure modes in each deployment phase.

引用

页数：7

共 25 条

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