UNKNOWN
Inversion of Gravity Fields from the Spacecraft Orbital Data Using an Adjoint Operator Approach
1999-04-19
Miscellaneous
No indication
English
Optimal Spacecraft Attitude Maneuvers via Adjoint Method
Trans Tech Publications | 2013
|Orbital Control of the Gravity Explorer Spacecraft: the Ion Propulsion Option
British Library Conference Proceedings | 1997
|Acting of Gravity Gradient and Jitter Accelerations on the On-Orbital Spacecraft
British Library Conference Proceedings | 1993
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