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Augmented Robust Cubature Kalman Filter Applied in Re-Entry Vehicle Tracking

  • School of Astronautics, Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

In this work, an improved cubature Kalman filter (CKF), called augmented robust CKF (ARCKF), for the reentry vehicle trajectory tracking is presented, in which the model strong nonlinearity, heavy-tailed measurement noise, and the non-independence of measurement noise in iterations are considered. Firstly, the derivative-free robust approach is employed instead of the conventional Huber's technique, thereby eliminating linearization errors and exhibiting robustness to measurement outliers. Secondly, the framework of iterated unscented Kalman filter is adopted to avoid linearization in the iterative measurement update, in which new cubature sample points are regenerated in each iteration, and then the probability density function is propagated through the measurement model. Furthermore, in the measurement update stage, the state vector is augmented with the measurement noise vector to address their correlation after the first iteration. To demonstrate the validity of the proposed algorithm, CKF, robust CKF (RCKF), and ARCKF are compared via Monte Carlo simulations. The results show that ARCKF performs with sufficient suitability in non-Gaussian noise environments and is superior in terms of target tracking accuracy.

Original languageEnglish
Title of host publication2021 IEEE Aerospace Conference, AERO 2021
PublisherIEEE Computer Society
ISBN (Electronic)9781728174365
DOIs
StatePublished - 6 Mar 2021
Externally publishedYes
Event2021 IEEE Aerospace Conference, AERO 2021 - Big Sky, United States
Duration: 6 Mar 202113 Mar 2021

Publication series

NameIEEE Aerospace Conference Proceedings
Volume2021-March
ISSN (Print)1095-323X

Conference

Conference2021 IEEE Aerospace Conference, AERO 2021
Country/TerritoryUnited States
CityBig Sky
Period6/03/2113/03/21

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