Hypersonic Entry Vehicle State Estimation Using High-Degree Cubature Kalman Filter (AIAA 2014-2383)
Conference, AIAA atmospheric flight mechanics ; 2014 ; Atlanta, GA
2014-01-01
12 pages
Includes bibliographical references and author index
Conference paper
English
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Hypersonic entry vehicle state estimation using nonlinearity-based adaptive cubature Kalman filters
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