Spacecraft Attitude and Body Rate Estimation with Four Star Sensor Heads: Concepts and Ground and On-Orbit Verification Results

Author:

Miyatake Katsumasa,Yoshikawa Shoji,Shimoji Haruhiko,Kawano Hiroyuki,Suzuki Takeshi,Kunii Yoshinori,Hama Kazumori,Oka Noriaki

Publisher

Elsevier BV

Subject

General Medicine

Reference6 articles.

1. Kawai, H. et al. (2006). Development of the new generation star tracker. JAXA-SP-05-008, 225-230, Japan Aerospace Exploration Agency (JAXA), Japan.

2. Kawano, H. et al. (2005). Suppression of sun interference in the star sensor baffling stray light by total internal reflection. Optical Systems Design 2005, SPIE Europe, Jena, Germany.

3. Development of SIS - satellite controller integrated with star sensors;Miyatake,2003

4. High-accuracy attitude determination for the X-ray satellite ROSAT;Rupp;J. Guidance Control Dynamics,1992

5. Spacecraft Attitude Determination and Control;Wertz,1978

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. Multi-Stage Star Image Identification Method of Three Field-of-View Star Sensor;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2019-06

2. Guide Star Selection for the Three-FOV Daytime Star Sensor;Sensors;2019-03-25

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