WIT Press


Cluster Geometry Recovery For Colocated Satellites

Price

Free (open access)

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

Keywords