Experimental Validation of Positive Adaptive-Control Approach for Spacecraft Proximity Maneuvers-Reference-Cited by-同舟云学术

Experimental Validation of Positive Adaptive-Control Approach for Spacecraft Proximity Maneuvers

Published:2021-11 Issue:6 Volume:34 Page:04021096
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Eun Youngho¹,Park Sang-Young²^ORCID,Lee Taeyang³^ORCID,Kim Geuk-Nam⁴^ORCID

Affiliation:

1. Ph.D. Student, Astrodynamics and Control Laboratory, Dept. of Astronomy, Yonsei Univ., Seoul 03722, Republic of Korea.

2. Professor, Astrodynamics and Control Laboratory, Dept. of Astronomy, Yonsei Univ., Seoul 03722, Republic of Korea (corresponding author). ORCID: .

3. Master Student, Astrodynamics and Control Laboratory, Dept. of Astronomy, Yonsei Univ., Seoul 03722, Republic of Korea. ORCID: .

4. Ph.D. Student, Astrodynamics and Control Laboratory, Dept. of Astronomy, Yonsei Univ., Seoul 03722, Republic of Korea. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001348

Reference28 articles.

1. Cho D.-M. D. Jung and P. Tsiotras. 2009. “A 5-dof experimental platform for autonomous spacecraft rendezvous and docking.” In Proc. AIAA Infotech@ Aerospace Conf. 1–20. Reston VA: American Institute of Aeronautics and Astronautics.

2. Daitx H. M. Schlotterer J. Whidborne and M. Sagliano. 2016. “Development of a combined attitude and position controller for a satellite simulator.” In Proc. 67th Int. Astronautical Congress (IAC). Paris: International Astronautical Federation.

3. Eun Y. 2018. “Development of a ground test facility for hardware-in-the-loop validation of multiple spacecraft operations.” Ph.D. thesis Dept. of Astronomy Yonsei Univ.

4. Development of a hardware-in-the-loop testbed to demonstrate multiple spacecraft operations in proximity

5. Application of the mini AERCam free flyer for orbital inspection

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