TY - GEN
T1 - A Weakly Model Dependent Control Scheme for a Class of Large-Scale Long-Range Aerospace Transportation Vehicle
AU - Chen, Haipeng
AU - Zhang, Feng
AU - Wang, Xiaowei
AU - Wei, Changzhu
N1 - Publisher Copyright:
© 2024 International Astronautical Federation, IAF. All rights reserved.
PY - 2024
Y1 - 2024
N2 - Global long-range transportation has been a new study focus in aerospace transportation field in recent years. This work mainly proposes a weakly model dependent control scheme to deal with control problems caused by large-scale long-range transportation, including aerodynamic parameter identification, low/dense-frequency vibration and complex disturbances. To this end, an autonomous prediction/correction strategy is designed incorporating off-line training and on-line incremental correction to obtain aerodynamic parameters; a joint design involving frequency identification and adaptive correction is given to attenuate complex vibration; and a synthesized robust control law, composed of disturbance observer, prescribed performance sliding-mode and robust feedback law, is then put forward enabling a satisfactory control performance. Besides the scheme design, the current study results and numerical simulations of three parts are given to show the effectiveness of the proposed techniques.
AB - Global long-range transportation has been a new study focus in aerospace transportation field in recent years. This work mainly proposes a weakly model dependent control scheme to deal with control problems caused by large-scale long-range transportation, including aerodynamic parameter identification, low/dense-frequency vibration and complex disturbances. To this end, an autonomous prediction/correction strategy is designed incorporating off-line training and on-line incremental correction to obtain aerodynamic parameters; a joint design involving frequency identification and adaptive correction is given to attenuate complex vibration; and a synthesized robust control law, composed of disturbance observer, prescribed performance sliding-mode and robust feedback law, is then put forward enabling a satisfactory control performance. Besides the scheme design, the current study results and numerical simulations of three parts are given to show the effectiveness of the proposed techniques.
KW - Large-scale tether deployment
KW - Space elevator
KW - control scheme
UR - https://www.scopus.com/pages/publications/86000006623
U2 - 10.52202/078373-0039
DO - 10.52202/078373-0039
M3 - 会议稿件
AN - SCOPUS:86000006623
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 352
EP - 357
BT - IAF Earth Observation Symposium - Held at the 75th International Astronautical Congress, IAC 2024
PB - International Astronautical Federation, IAF
T2 - 2024 IAF Space Transportation Solutions and Innovations Symposium at the 75th International Astronautical Congress, IAC 2024
Y2 - 14 October 2024 through 18 October 2024
ER -