Finite-Time Backstepping Attitude Controller for First-Stage Booster Recovery by Parafoil System-Reference-Cited by-同舟云学术

Finite-Time Backstepping Attitude Controller for First-Stage Booster Recovery by Parafoil System

Published:2024-01 Issue:1 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Xing Xiaojun¹^ORCID,Feng Lei²^ORCID,Chen Mengping³,Gong Qianchao²^ORCID,Guo Yiming⁴

Affiliation:

1. Associate Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, China (corresponding author). ORCID: .

2. Master’s Student, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, China. ORCID:

3. Master’s Student, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, China.

4. Ph.D. Student, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710129, China.

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/JAEEEZ.ASENG-5340

Reference27 articles.

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3. Gao H. 2014. “Research on autonomous homing trajectory planning and control of parafoil system.” Ph.D. thesis School of Computer and Control Engineering Nankai Univ.

4. Gockel W. 1997. “Concept studies of an autonomous GNC system for gliding parachute.” In Proc. 14th Aerodynamic Decelerator Systems Technology Conf. 1465. Reston VA: American Institute of Aeronautics and Astronautics.

5. Goodrick T. 1975. “Theoretical study of the longitudinal stability of high-performance gliding airdrop systems.” In Proc. 5th Aerodynamic Deceleration Systems Conf. 1394. Reston VA: American Institute of Aeronautics and Astronautics.