The paper is concerned with the phase of the geosynchronous mission termed station acquisition, which involves the maneuvering of a spacecraft to its geostationary longitude by means of the spacecraft propulsion system. An algorithm which assists in maneuver planning is described, and examples of its use are presented. The algorithm can be applied when sequences of more than three maneuvers are to be expected. While, in general, three maneuvers are sufficient to achieve the desired end conditions when orbital mechanics are the only consideration, operational considerations may add constraints resulting in an increased number of maneuvers required.
A geostationary longitude acquisition planning algorithm
Astrodynamics Specialist Conference
1977-09-01
Conference paper
No indication
English
Algorithm for Autonomous Longitude and Eccentricity Control for Geostationary Spacecraft
Online Contents | 2003
|British Library Conference Proceedings | 2002
|