State Vector Determination By A Single Tracking Satellite

Details State Vector Determination By A Single Tracking Satellite State Vector Determination By A Single Tracking Satellite

2007-05-08

arxiv.org/abs/0705.1155v1

Astronomy and Astrophysics

Astrophysics

Scientific paper

Using only a single tracking satellite capable of only range measurements to
an orbiting object in an unknown Keplerian orbit, it is theoretically possible
to calculate the orbit and a current state vector. In this paper we derive an
algorithm that can perform this calculation.

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