GNC concept for automated landing of a large parafoil-Reference-Cited by-同舟云学术

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GNC concept for automated landing of a large parafoil

Published:1997-06-03 Issue: Volume: Page:
ISSN:
Container-title:14th Aerodynamic Decelerator Systems Technology Conference
language:
Short-container-title:

Author:

Soppa Uwe¹,Strauch Hans¹,Goerig Laurent²,Belmont Jean²,Cantinaud Olivier²,Soppa Uwe¹,Strauch Hans¹,Goerig Laurent²,Belmont Jean²,Cantinaud Olivier²

Affiliation:

1. DASA RI, Bremen, Germany

2. Dassault Aviation, St. Cloud, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1464

Reference2 articles.

1. P.M.Hollestelle:The ElectricalArchitecture of aParafoil TechnologyDemonstrator;AIAA Paper 97-1467

Cited by 12 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. Improved A* Algorithm and Bézier Curve Optimization-Based Path Plan for the Landing Control of Parafoil;2023 IEEE International Conference on Unmanned Systems (ICUS);2023-10-13

2. Multi-Phase Homing Trajectory Planning and Control for Parafoil-Payload System;2023 42nd Chinese Control Conference (CCC);2023-07-24

3. Online Trajectory Planning for Parafoil First-Stage Booster System in Complex Wind Field;Journal of Aerospace Engineering;2023-07

4. Research on parafoil optimal flight path planning algorithm for precise recovery of sub-stage booster of rocket;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2022-02

5. Autonomous parafoil precision landing using convex real-time optimized guidance and control;CEAS Space Journal;2022-01-18

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