A new derivation of the GYROLITE stability criterion is presented. It is confirmed that, for the satellite to have a stable attitude, the spinning part must have a favorable inertia ratio.
The GYROLITE: Is it Unstable?
IEEE Transactions on Aerospace and Electronic Systems ; AES-15 , 4 ; 565-567
1979-07-01
373681 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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