Mahalanobis distance-based fading cubature Kalman filter with augmented mechanism for hypersonic vehicle INS/CNS autonomous integration-Reference-Cited by-同舟云学术

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Mahalanobis distance-based fading cubature Kalman filter with augmented mechanism for hypersonic vehicle INS/CNS autonomous integration

Published:2021-10 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

GAO Bingbing,LI Wenmin,HU Gaoge,ZHONG Yongmin,ZHU Xinhe

Funder

National Natural Science Foundation of China

Natural Science Basic Research Program of Shaanxi Province

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference34 articles.

1. Hypersonic boost-glide vehicle strapdown inertial navigation system/global positioning system algorithm in a launch-centered earth-fixed frame;Chen;Aerosp Sci Technol,2020

2. Robust tracking control of hypersonic flight vehicles: A continuous model-free control approach;Bu;Acta Astronaut,2019

3. Comparison of geomagnetic aided navigation algorithms for hypersonic vehicles;Chen;J Zhejiang Univ Sci A,2020

4. In-motion alignment for a velocity-aided SINS with latitude uncertainty;Fu;IEEE/ASME Trans Mechatron,2020

5. Maximum correntropy square-root cubature Kalman filter with application to SINS/GPS integrated systems;Liu;ISA Trans,2018

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