Design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control
In this paper, the design and implementation of hardware-in-the-loop (HIL) test-bed for spacecraft attitude control are presented with respect to the practical consideration. This test-bed includes an air bearing 3-DOF table, Helmholtz coil, sun simulator, orbit simulator, reaction wheels and torqro...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2019-08-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_184934_a1f9e8803375c97f0d0f5c490470d764.pdf |