Terminal Trajectory Planning for the First-Stage Booster of Rocket Recovery by Parafoil System in Complex Obstacle Environments-Reference-Cited by-同舟云学术

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Terminal Trajectory Planning for the First-Stage Booster of Rocket Recovery by Parafoil System in Complex Obstacle Environments

Published:2024-08 Issue:4 Volume:60 Page:4979-4993
ISSN:0018-9251
Container-title:IEEE Transactions on Aerospace and Electronic Systems
language:
Short-container-title:IEEE Trans. Aerosp. Electron. Syst.

Author:

Xing Xiaojun¹^ORCID,Wang Rui¹^ORCID,Gong Qianchao¹^ORCID,Xiao Bing¹^ORCID

Affiliation:

1. College of Automation, Northwestern Polytechnical University, Xi'an, China

Funder

National Natural Science Foundation of China

Xi'an Science and Technology Plan Project

Industry-University-Research Innovation Fund of Chinese Universities

Natural Science Basic Research Program of Shaanxi Province

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/7/10631738/10487804.pdf?arnumber=10487804

Reference31 articles.

1. Development status and prospect of reusable space transportation system in China;Long;Space Int.,2019

2. Recent Developments of Experimental Winged Rocket: Autonomous Guidance and Control Demonstration Using Parafoil

3. Modeling and research of a multi-stage parachute system for the booster recovery

4. Design and optimization in multiphase homing trajectory of parafoil system

5. Controlled recovery of payloads at large glide distances, using the para-foil.

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