Development of Hardware-in-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer

Author:

Shim Hanjoon1ORCID,Kim O-Jong2,Park Minhuck3,Choi Minkyu4,Kee Changdon1ORCID

Affiliation:

1. Department of Aerospace Engineering, Seoul National University, Seoul, South Korea

2. Department of Aerospace Engineering, Sejong University, Seoul, South Korea

3. GNSS Research and Development Center, Danam Systems Inc., Anyang, South Korea

4. Device Solutions Division, Samsung Electronics, Hwaseong, South Korea

Funder

Future Space Navigation & Satellite Research Center through the National Research Foundation funded by the Ministry of Science and ICT, the Republic of Korea

Institute of Advanced Aerospace Technology at Seoul National University

The Institute of Engineering Research at Seoul National University provided research facilities for this work

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

General Engineering,General Materials Science,General Computer Science,Electrical and Electronic Engineering

Reference61 articles.

1. CubeSat Three Axis Simulator(CubeTAS)

2. HILS verification of low Earth orbit cube-satellite attitude determination and control system using helmholtz cage;shim,2019

3. The development of a software and hardware-in-the-loop test system for ITU-PSAT II nano satellite ADCS;ure;Proc Aerosp Conf,2011

4. Kalman filtering for spacecraft attitude estimation

5. Survey of worldwide pico- and nanosatellite missions, distributions and subsystem technology

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