Abstract
Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance, navigation and robust control are considered and elaborated methods are presented for their solving.
Original language | English |
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Pages (from-to) | 222-227 |
Number of pages | 6 |
Journal | IFAC-PapersOnLine |
Volume | 28 |
Issue number | 9 |
DOIs | |
Publication status | Published - 1 Jul 2015 |
Event | 1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 - Seville, Spain Duration: 10 Jun 2015 → 12 Jun 2015 |
Bibliographical note
Publisher Copyright:© 2015, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
Keywords
- Attitude control
- Guidance
- Mini-satellite
- Navigation