Analysis of RAE-B attitude data

Computer Science – Performance

Scientific paper

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Attitude (Inclination), Explorer 49 Satellite, Orbital Mechanics, Computerized Simulation, Data Smoothing

Scientific paper

Attempts made to obtain a description of the in-orbit dynamic behavior of the RAE-B spacecraft and account for the discrepancies between predicted and actual in-orbit performance are reported. In particular, attitude dynamics during the final despin operations in lunar orbit, throughout all deployment operations, and into the final steady state mission mode were investigated. Attempts made to match computer simulation results to the observed equilibrium data are discussed. Due to a damaged antenna boom and the unavailability of sufficient attitude and dynamics data, most of the objectives were not realized.

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