Applying a novel extended Kalman filter to missile-target interception with APN guidance law: A benchmark case study

Control Engineering Practice

Volumn 18, Issue 2, 2010, Pages 159-167

  Pan, Shuwen ^a   Su, Hongye ^a   Chu, Jian ^a   Wang, Hong ^a  

^a ZHEJIANG UNIVERSITY   (China)

Author keywords

Augmented proportional navigation guidance law; Extended Kalman filter; Missile target interception; Nonlinear filtering; Unknown inputs

Indexed keywords

AUGMENTED PROPORTIONAL NAVIGATION; AUGMENTED PROPORTIONAL NAVIGATION GUIDANCE LAW; BENCHMARK CASE STUDIES; FEED THROUGH; GUIDANCE LAWS; MEASUREMENT NOISE; MODEL UNCERTAINTIES; PRIOR INFORMATION; RECURSIVE APPROACH; SIMULATION RESULT; STATE VECTOR; TARGET ACCELERATION; TARGET ENGAGEMENT SYSTEMS; UNKNOWN INPUTS; WEIGHTED LEAST SQUARES ESTIMATION;

ELECTRONIC GUIDANCE SYSTEMS; ESTIMATION; EXTENDED KALMAN FILTERS; MISSILES; MOBILE TELECOMMUNICATION SYSTEMS; NAVIGATION; NONLINEAR FILTERING; POSITION CONTROL; UNCERTAINTY ANALYSIS;

TARGETS;

EID: 76749112420     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.conengprac.2009.09.010     Document Type: Article

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