Shape Parameters Estimation of IKAROS Solar Sail Using In-Flight Attitude Determination Data-Reference-Cited by-同舟云学术

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Shape Parameters Estimation of IKAROS Solar Sail Using In-Flight Attitude Determination Data

Published:2011-04-04 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
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Author:

Tsuda Yuichi¹,Saiki Takanao¹,Funase Ryu¹,Shirasawa Yoji²,Mimasu Yuya³

Affiliation:

1. Japan Aerospace Exploration Agency (JAXA)

2. University of Tokyo

3. Kyushu University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1889

Reference10 articles.

1. J.Kawaguchi,"ASolarPowerSailMissionforAJovianOrbiterandTrojanAsteroidFlybys,"COSPAR04-A-01655,2004.

2. Y. Tsuda, O.Mori, R.Funase, H. Sawada, T.Yamamoto, T.Saiki,T.EndoandJ. Kawaguchi,"FlightStatusof IKAROSDeep Space SolarSailDemonstrator,"61stInternational AstronauticalCongress, IAC-10-A3.6.8, Prague, Sep.27-Oct.1, 2010.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Shape Estimation of Gossamer Structures Using Distributed Sun-Angle Measurements;Journal of Spacecraft and Rockets;2018-03

2. Design Criteria of Spinning Solar Sail Surface Based on Attitude Dynamics;AIAA/AAS Astrodynamics Specialist Conference;2012-08-13

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