Cluster Geometry Recovery For Colocated Satellites
Price
Free (open access)
Transaction
Volume
22
Pages
9
Published
1996
Size
583 kb
Paper DOI
10.2495/DCSS960351
Copyright
WIT Press
Author(s)
S. Hardacre
Abstract
Hill's equations of relative motion are applied to the problem of re-initialising the relative orbit of a cluster of Geosynchronous satellites which have deviated from their nominal relative orbits to such an extent that there exists an unacceptably high collision or telecommunication interference risk. A solution is presented for satellites possessing thruster capability along two perpendicular axes, the longitudinal direction and the latitudinal direction, which correspond to the burn directions used for East-West and North-South station keeping of GEO satellites. Absolute positional recovery with reference to a geocentric inertial frame is not considered. 1 Introduction The World Radio Administrative Conference of 1977 (WARC 77) was held to discuss direct broadcast satellite services. During the conference a plan for the allocation
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