Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1713215 | Journal of Systems Engineering and Electronics | 2006 | 4 Pages |
Abstract
A conditional boost-phase trajectory estimation method based on ballistic missile (BM) information database and classification is developed to estimate and predict boos-phase BM trajectory. The main uncertain factors to describe BM dynamics equation are reduced to the control law of trajectory pitch angle in boost-phase. After the BM mass at the beginning of estimation, the BM attack angle and the modification of engine thrust denoting BM acceleration are modeled reasonably, the boost-phase BM trajectory estimation with ground based radar is well realized. The validity of this estimation method is testified by computer simulation with a typical example.
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Physical Sciences and Engineering
Engineering
Control and Systems Engineering
Authors
Tang Yuyan, Huang Peikang,