SpaceWire-based thermal-infrared imager system for asteroid sample return mission HAYABUSA2

Author:

Hihara Hiroki1,Iwase Kaori1,Sano Junpei1,Otake Hisashi2,Okada Tatsuaki2,Funase Ryu3,Kashikawa Ryoichi1,Higashino Isamu1,Masuda Tetsuya4

Affiliation:

1. NEC TOSHIBA Space Systems, Ltd., 1–10 Nisshin-cho, Fuchu, Tokyo 183-8551, Japan

2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa 252-5210, Japan

3. University of Tokyo, Department of Aeronautics and Astronautics, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan

4. NEC Corporation, 1–10 Nisshin-cho, Fuchu, Tokyo 183-8551, Japan

Publisher

SPIE-Intl Soc Optical Eng

Subject

General Earth and Planetary Sciences

Cited by 12 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. Design of Infrared Thermal Imager Calibration System;2021 IEEE 15th International Conference on Electronic Measurement & Instruments (ICEMI);2021-10-29

2. Onboard signal processing system of HAYABUSA2;Infrared Remote Sensing and Instrumentation XXVIII;2020-08-20

3. Atomic Switch FPGA: Application for IoT Sensing Systems in Space;Atomic Switch;2020

4. Performance evaluation of the optical navigation electronics of HAYABUSA2;SPIE Future Sensing Technologies;2019-11-12

5. Applications of Reconfigurable Processors as Embedded Automatons in the IoT Sensor Networks in Space;VLSI Design and Test for Systems Dependability;2018-07-21

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