TY - JOUR
T1 - Along-track deployment control of space tether system for SAR-GMTI mission
AU - Li, Linxiao
AU - Li, Aijun
AU - Lu, Hongshi
AU - Wang, Changqing
N1 - Publisher Copyright:
© 2024 IAA
PY - 2025/1
Y1 - 2025/1
N2 - Global, 24/7, and all-weather Synthetic Aperture Radars (SARs) are optimal platforms for Ground Moving Target Indication (GMTI) missions, and the tether constraint provides a stable mechanic connection for such configurations. To fulfill the requirements of such missions, the Space Tether System (STS) must be deployed to horizontal positions to form the necessary along-track interference baseline, which is unstable relative to traditional vertical positions and has not received adequate focus. To deal with this problem, this study focuses on the deployment control of the STS to the unstable horizontal positions. Firstly, the properties of the STS at the horizontal position are analyzed, and a synthetic criterion of measurement error is defined based on the observation principle of the GMTI mission. Secondly, two deployment control strategies are proposed, and corresponding desired trajectories are generated by considering two occasions respectively. In the end, considering the instability of horizontal positions, an adaptive closed-loop controller is designed utilizing the backstepping method to address gravitational moment and other disturbances. Simulations demonstrate that the system can successfully attain the desired horizontal positions under both deployment strategies, and the designed controller can quickly track trajectories under initial state errors and external disturbances.
AB - Global, 24/7, and all-weather Synthetic Aperture Radars (SARs) are optimal platforms for Ground Moving Target Indication (GMTI) missions, and the tether constraint provides a stable mechanic connection for such configurations. To fulfill the requirements of such missions, the Space Tether System (STS) must be deployed to horizontal positions to form the necessary along-track interference baseline, which is unstable relative to traditional vertical positions and has not received adequate focus. To deal with this problem, this study focuses on the deployment control of the STS to the unstable horizontal positions. Firstly, the properties of the STS at the horizontal position are analyzed, and a synthetic criterion of measurement error is defined based on the observation principle of the GMTI mission. Secondly, two deployment control strategies are proposed, and corresponding desired trajectories are generated by considering two occasions respectively. In the end, considering the instability of horizontal positions, an adaptive closed-loop controller is designed utilizing the backstepping method to address gravitational moment and other disturbances. Simulations demonstrate that the system can successfully attain the desired horizontal positions under both deployment strategies, and the designed controller can quickly track trajectories under initial state errors and external disturbances.
KW - Adaptive backstepping control
KW - Along-track deployment
KW - Horizontal position
KW - SAR-GMTI
KW - Space tether system
UR - http://www.scopus.com/inward/record.url?scp=85206923950&partnerID=8YFLogxK
U2 - 10.1016/j.actaastro.2024.10.041
DO - 10.1016/j.actaastro.2024.10.041
M3 - 文章
AN - SCOPUS:85206923950
SN - 0094-5765
VL - 226
SP - 102
EP - 111
JO - Acta Astronautica
JF - Acta Astronautica
ER -