Hardware-in-loop-simulator for InnoSAT attitude control system
After launching, the initial condition of satellite is unknown and tends to be in a tumbling state. At this moment, the satellite needs to reduce the tumbling rate so that the satellite can enter a stable and unruffled state. The satellite also must maintain a certain attitude while orbiting in orde...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Insight Society
2016
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| Subjects: | |
| Online Access: | View Fulltext in Publisher View in Scopus |