Orbit determination from two position vectors and periapsis radius, introducing polar equation for conic to obtain solution
Orbit determination from two position vectors and periapsis radius
1969-08-01
Miscellaneous
No indication
English
Optimizing Periapsis-Raise Maneuvers using Low-Thrust Propulsion (AAS 08-298)
British Library Conference Proceedings | 2008
|Electromagnetic waves observed by Venus Express at periapsis: Detection and analysis techniques
Online Contents | 2008
|Reconstructing Time of Periapsis from Spacecraft Telemetry During Magellan Aerobraking (AAS 94-054)
British Library Conference Proceedings | 1994
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