A typical GYROLITE spacecraft recently designed by this author is described. It is shown that, for the satellite to have a stable attitude, the spinning part must have a favorable inertia ratio.
The GYROLITE: a new generation synchronous satellite
Gyrolite, ein Synchronsatellit der neuen Generation
1977
3 Seiten, 1 Bild, 1 Tabelle, 2 Quellen
Article (Journal)
English
The Gyrolite: A New Generation Synchronous Satellite
IEEE | 1977
|IEEE | 1979
|A necessary and sufficient condition for Gyrolite stability
Tema Archive | 1980
|