| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 713113 | IFAC-PapersOnLine | 2015 | 6 Pages |
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.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
