Attitude Stability Analysis and Configuration Design of Pyramid Drag Sail for Deorbit Missions-Reference-Cited by-同舟云学术

Attitude Stability Analysis and Configuration Design of Pyramid Drag Sail for Deorbit Missions

Published:2022-11 Issue:6 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Jingrui¹,Zhang Ruonan²,Yang Keying³^ORCID

Affiliation:

1. Professor, School of Aerospace Engineering, Beijing Institute of Technology, 5th South Zhongguancun St., Beijing 100081, PR China.

2. Master’s Student, School of Aerospace Engineering, Beijing Institute of Technology, 5th South Zhongguancun St., Beijing 100081, PR China.

3. Postdoctoral, School of Aerospace Engineering, Beijing Institute of Technology, 5th South Zhongguancun St., Beijing 100081, PR China (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001479

Reference45 articles.

1. DragSail systems for satellite deorbit and targeted reentry

2. Variable-Geometry Solar Sailing: The Possibilities of the Quasi-Rhombic Pyramid

3. Solar electric propulsion orbital debris ferry, vehicle concept and reference mission

4. Attitude Stability and Altitude Control of a Variable-Geometry Earth-Orbiting Solar Sail

5. Felicetti L. P. Harkness and M. Ceriotti. 2017. “Attitude and orbital dynamics of a variable-geometry spinning solar sail in Earth orbit.” In Proc. 4th Int. Symp. on Solar Sailing. Kyoto Japan: The Kyoto Convention & Visitors Bureau.

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