Dynamic-model-based closed-loop guidance and control for heavy parafoil system precision landing-Reference-Cited by-同舟云学术

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Dynamic-model-based closed-loop guidance and control for heavy parafoil system precision landing

Published:2024-03 Issue: Volume:146 Page:108964
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wei Zhenyu^ORCID,Gao Yan^ORCID,Shao Zhijiang,Wang Cong^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference45 articles.

1. Advanced features for autonomous parafoil guidance, navigation and control;Jann,2005

2. Bézier curve path planning for parafoil terminal guidance;Fowler;J. Aerosp. Inform. Syst.,2014

3. Controlled recovery of payloads at large glide distances, using the para-foil;Knapp;J. Aircr.,1968

4. Autonomous large parafoil guidance, navigation, and control system design status;Carter,2007

5. Testing of parafoil autonomous guidance, navigation & control for x-38;Strahan,2003

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Parafoil System Cooperative Recovery: A Coordinated Distributed NMPC Approach;IEEE Transactions on Aerospace and Electronic Systems;2024-08

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