Orbit determination and control for the AMPTE UK satellite.

Details Orbit determination and control for the AMPTE UK satellite. Orbit determination and control for the AMPTE UK satellite.

Aug 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986asdy.conf.1099s&link_type=abstract

Astrodynamics 1985, p. 1099 - 1117

Astronomy and Astrophysics

Astronomy

Artificial Satellites:Orbit Determination, Orbit Determination:Artificial Satellites

Scientific paper

The procedures used for orbit determination and control of the AMPTE (Active Magnetospheric Particle Tracer Explorers) UK satellite (UKS) are described and the operational experience is reviewed. In particular, details are given about how the separation between the UKS and the companion Ion Release Module satellite was controlled to meet the scientific requirements of the AMPTE mission, utilising a cold gas thruster system on board UKS.

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