A mathematical model is reported for determination of satellite position, velocity, and attitude using landmark coordinates as observables. This model, although developed with respect to earth stabilized missions, Tiros-N and Nimbus-G in particular, is applicable to any earth stabilized satellite in general.
Utilization of landmark data in attitude/orbit determination
1975-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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