Studies on Magnetic Attitude Control System for the REIMEI Microsatellite-Reference-Cited by-同舟云学术

Studies on Magnetic Attitude Control System for the REIMEI Microsatellite

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference and Exhibit
language:
Short-container-title:

Author:

Sakai Shin-ichiro¹,Fukushima Yosuke¹,Saito Hirobumi¹,Kaneda Ryosuke²

Affiliation:

1. Japan Aerospace Exploration Agency

2. University of Tokyo

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6450

Reference20 articles.

1. (b)

2. (b)

3. k2 -2.789 ×10-32.789 ×10-3k1 4.933 ×10-5- 4.933 ×10-5k0 3.721 ×10-7- 3.721 ×10-7l3 1.0 1.0 l2 0.2217 0.2217 l1 0.01728 0.01728 I 4.08 [Nm2] 3.839 [Nm2] hz 0.5 [Nms] S(s)

4. T(s) -100 -80 -60 -40 -20 0 20 10 10 10 10 10 -4 -3 -2 -1 0

5. Fig. 8 plots the attitude response during the maneuver to shift z-body axis direction. Magnetic torque of MTQs drives this maneuver, and the rate is about 10-20 degrees per hour. Therefore, typical time sequence of MAC aurora imaging is as follows:

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