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
IEEE Transactions on Aerospace and Electronic Systems ; AES-13 , 6 ; 651-653
1977-11-01
1594266 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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