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Iterated Sigma-Point Kalman Filtering for Trajectory ReconstructionTwo second-order Kalman filtering methods are added to the New Statistical Trajec-tory Estimation Program (NewSTEP). The two filters are of the class of Sigma-Point Kalman Filters, namely the Unscented Kalman Filter and the Divided Difference Filter. Both filters are implemented with an iterative measurement update step. Results from simulation test case and a flight data test case are provided to show the filter performance. The results indicate that the new second-order filters pro-duce trajectory estimates with reduced uncertainties when compared to the existing first-order filtering method.
Document ID
20240001235
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Sophia Vedvik
(University of Minnesota Minneapolis, United States)
Christopher D Karlgaard
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
January 26, 2024
Publication Date
March 1, 2024
Subject Category
Aerodynamics
Funding Number(s)
WBS: 981698.01.02.23.17
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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