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8 June 1994 Orbital debris trajectory error modeling
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Abstract
A computer simulation which estimates statistical orbital debris trajectory error arising from uncertainty of debris size, composition, geometry, and tumbling rate and also of atmospheric density is discussed. The ramification of the simulation results to debris accuracy requirements determined from maneuver rate constraints is examined.
© (1994) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Brian A. Bourgeois and Kent Dekome "Orbital debris trajectory error modeling", Proc. SPIE 2214, Space Instrumentation and Dual-Use Technologies, (8 June 1994); https://doi.org/10.1117/12.177680
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