TY - GEN
T1 - “Xiyuan” Space Debris Removal demonstration mission
AU - Yuan, Jianping
AU - Yuan, Jing
AU - Li, Shulong
AU - Yang, Dong
N1 - Publisher Copyright:
Copyright © 2024 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2024
Y1 - 2024
N2 - Growing number of space debris poses a significant threat to the security of in orbit satellites. It is importance to ensure a safe and sustainable orbital space environment through active space debris mitigation programs. Sanyuan Space - a startup venture engaged in on-orbit services, aims to provide on-orbit servicing including active space debris removal, on-orbit refueling, on-orbit maintenance, and other services, in collaboration with School of Astronautics, Northwestern Polytechnical University, plans to launch an satellite “Xiyuan” in 2025 to demonstrate key technologies for space debris removal, such as target capture technology, relative navigation technology, multidimensional information perception technology, and close Proximity technology, etc. This demonstration is divided into two stages. The first stages involves target pose estimation, close proximity and capture of a self-carried mock target. The second stage will implement orbit mannuver and relative guidance to approach and inspect a resident space object. This paper introduces the mission design, highlights, and key technologies of “Xiyuan”.
AB - Growing number of space debris poses a significant threat to the security of in orbit satellites. It is importance to ensure a safe and sustainable orbital space environment through active space debris mitigation programs. Sanyuan Space - a startup venture engaged in on-orbit services, aims to provide on-orbit servicing including active space debris removal, on-orbit refueling, on-orbit maintenance, and other services, in collaboration with School of Astronautics, Northwestern Polytechnical University, plans to launch an satellite “Xiyuan” in 2025 to demonstrate key technologies for space debris removal, such as target capture technology, relative navigation technology, multidimensional information perception technology, and close Proximity technology, etc. This demonstration is divided into two stages. The first stages involves target pose estimation, close proximity and capture of a self-carried mock target. The second stage will implement orbit mannuver and relative guidance to approach and inspect a resident space object. This paper introduces the mission design, highlights, and key technologies of “Xiyuan”.
KW - ADR
KW - relative navigation
KW - rendezvous proximity operations
KW - space operation demonstration
KW - Xiyuan
UR - http://www.scopus.com/inward/record.url?scp=85218464911&partnerID=8YFLogxK
U2 - 10.52202/078367-0063
DO - 10.52202/078367-0063
M3 - 会议稿件
AN - SCOPUS:85218464911
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 591
EP - 595
BT - IAF Space Operations Symposium - Held at the 75th International Astronautical Congress, IAC 2024
PB - International Astronautical Federation, IAF
T2 - 2024 IAF Space Operations Symposium at the 75th International Astronautical Congress, IAC 2024
Y2 - 14 October 2024 through 18 October 2024
ER -