Missile Guidance Law Estimation Using Modified Interactive Multiple Model Filter

This paper presents an interactive multiple-model-based guidance law estimation filter. An antiship missile’s threat index, such as the remaining time of flight and impact angle, can be estimated by using the guidance law estimation filter. The filter bank of the filter was composed of models based...

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 2014-03, Vol.37 (2), p.484-496
Hauptverfasser: Yun, Joongsup, Ryoo, Chang-Kyung
Format: Artikel
Sprache:eng
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