Attitude Stabilization for the Nano Remote Sensing Satellite PRISM

Author:

Inamori Takaya1,Shimizu Kensuke2,Mikawa Yoshinori2,Tanaka Toshiki2,Nakasuka Shinichi3

Affiliation:

1. Graduate Student, Intelligent Space Systems Laboratory 608, Dept. of Aeronautics and Astronautics, Univ. of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan (corresponding author).

2. Graduate Student, Intelligent Space Systems Laboratory 608, Dept. of Aeronautics and Astronautics, Univ. of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan.

3. Professor, Intelligent Space Systems Laboratory 308, Dept. of Aeronautics and Astronautics, Univ. of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference13 articles.

1. Bar-Itzhack I. Y. and Harman R. (2004). “Implicit and explicit spacecraft gyro calibration.” Proc. AIAA GNC Conf. Exhibit AIAA Reston VA.

2. Real-Time Attitude-Independent Three-Axis Magnetometer Calibration

3. Technology demonstration on University of Tokyo's pico-satellite “XI-V” and its effective operation result using ground station network

4. Heidt H. Puig-Suari J. Moore A. S. Nakasuka S. and Twiggs R. J. (2000). “CubeSat: A new generation of picosatellite for education and industry low-cost space experimentation.” Proc. 14th Annual/Utah State Univ. Conf. on Small Satellites AIAA Reston VA.

5. Inamori T. et al. (2009). “Attitude determination and control system in pico-satellite for remote-sensing and innovative space missions (PRISM).” Proc. 27th Int. Symp. on Space Technology and Science Japan Society for Aeronautical and Space Sciences Tokyo.

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