Sensitivity Analysis of EKF and UKF in GPS/INS Sensor Fusion-Reference-Cited by-同舟云学术

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Sensitivity Analysis of EKF and UKF in GPS/INS Sensor Fusion

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
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Author:

Rhudy Matthew¹,Gu Yu¹,Gross Jason¹,Napolitano Marcello¹

Affiliation:

1. West Virginia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6491

Reference30 articles.

1. Fiorenzani,T.,etal."ComparativeStudyofUnscentedKalmanFilterandExtendedKalmanFilterforPosition/Attitude Estimation in Unmanned Aerial Vehicles," IASI-CNR, R.08-08,2008.

2. Unscented Filtering for Spacecraft Attitude Estimation

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1. Maximum correentropy-based robust Square-root Cubature Kalman Filter for vehicular cooperative navigation;Scientific Reports;2023-12-27

2. A Novel Vehicle Localization Method Based on Adaptive Singular Spectrum Analysis Using Low-Cost INS/GNSS;IEEE Access;2023

3. Airborne Vision Based Target Motion State Estimation for UAV Aerial Docking;Lecture Notes in Electrical Engineering;2023

4. Relaxation of Stability Requirements for Extended Kalman Filter Stability within GPS/INS Attitude Estimation;AIAA Guidance, Navigation, and Control Conference;2014-01-10

5. Relaxation of Initial Error and Noise Bounds for Stability of GPS/INS Attitude Estimation;AIAA Guidance, Navigation, and Control Conference;2012-08-13

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