Covariance Matrix Transformation Method for Absolute/Relative Measurements Fusion of Vision/IMU/GNSS Integration in Parafoil Landing-Reference-Cited by-同舟云学术

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Covariance Matrix Transformation Method for Absolute/Relative Measurements Fusion of Vision/IMU/GNSS Integration in Parafoil Landing

Published:2024-05-15 Issue:10 Volume:24 Page:16673-16687
ISSN:1530-437X
Container-title:IEEE Sensors Journal
language:
Short-container-title:IEEE Sensors J.

Author:

Wang Jingqi¹^ORCID,Xiong Zhi¹^ORCID,Zhao Yao¹^ORCID,Ding Yiming¹^ORCID,Liu Yihan¹,Wang Huanjin²^ORCID,Yan Luqi²^ORCID

Affiliation:

1. Navigation Research Center, School of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

2. Key Laboratory of Unsteady Aerodynamics and Flow Control, Ministry of Industry and Information Technology, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

Funder

Chinese National Programs for Fundamental Strengthening Research

National Natural Science Foundation of China

Aeronautic Science Foundation of China

2023 Fundamental Research Funds for the Central Universities of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/7361/10530892/10500326.pdf?arnumber=10500326

Reference31 articles.

1. Simulation and Comparison of Control Laws for the Landing of an autonomous Parafoil under Adverse Conditions

2. Development and Testing of a Control System for the Automatic Flight of Tethered Parafoils

3. Landing Guidance Strategy of Space Rider

4. Guided-Airdrop Vision-Based Navigation

5. Vision-Based Terrain Relative Navigation on High Altitude Balloon and Sub-Orbital Rocket

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