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Adaptive Filtering Approach for Missile Flight Test Trajectory Determination Under Multiple Station Measuring
Pages: 17-22
Year: Issue:  2
Journal: Aerospace Control

Keyword:  Trajectory analysis Adaptive filter Measurement;
Abstract: In this paper, an adaptive filtering approach is applied to determine missile fight ttest trajectory under multiple station measuring. The trajectory estimation with higd precision is obtained by compensating adaptively systematic measurement errors and acceleration randoem noise statistics in full consideratish of the information provided by dynamic model of missile fight. The computation resolts indicate that the interactive way to estimate fight states and systematic measurement errors is effective in data processing procedure.
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