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This research investigated relative orbit determination of individual satellites within a cluster, focusing on instances whena maneuver has been detected or suspected. Developed using non-linear least squares estimation, the maneuver modelestimates magnitude, direction, and time of a suspected maneuver. Observations for the DirecTV 4S and AMC-4 satellitecollocation were obtained from the Air Force Maui Optical and Supercomputing (AMOS) site consisting of differentialright ascension and declination. Dynamics are modeled using Hill's equations.

Produktbeschreibung
This research investigated relative orbit determination of individual satellites within a cluster, focusing on instances whena maneuver has been detected or suspected. Developed using non-linear least squares estimation, the maneuver modelestimates magnitude, direction, and time of a suspected maneuver. Observations for the DirecTV 4S and AMC-4 satellitecollocation were obtained from the Air Force Maui Optical and Supercomputing (AMOS) site consisting of differentialright ascension and declination. Dynamics are modeled using Hill's equations.
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