Abstract
Contemporary land-survey satellites are placed onto the orbit altitudes from 600 up to 1000 km. For such spacecraft we consider some principal problems on the spacecraft attitude digital and pulse-width control and present elaborated methods for in-flight identification, verification and management of attitude control system with animation of satellite motion.
Original language | English |
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Pages (from-to) | 833-838 |
Number of pages | 6 |
Journal | IFAC-PapersOnLine |
Volume | 49 |
Issue number | 12 |
DOIs | |
Publication status | Published - 2016 |
Bibliographical note
Publisher Copyright:© 2016
Keywords
- attitude control system
- in-flight management
- land-survey satellite