Robust control of the servo system of Leighton Chajnantor Telescope under high wind speed

被引:7
作者
Chen, Weirui [1 ]
Wang, Zheng [1 ]
机构
[1] Southeast Univ, Sch Automat, Nanjing 210096, Peoples R China
来源
MODELING, SYSTEMS ENGINEERING, AND PROJECT MANAGEMENT FOR ASTRONOMY X | 2022年 / 12187卷
关键词
Leighton Chajnantor Telescope (LCT); Caltech Submillimeter Observatory telescope (CSO); wind disturbance; pointing accuracy; servo control system; robust control; H-infinity control; LQG CONTROLLER; ANTENNAS;
D O I
10.1117/12.2628687
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The Caltech Submillimeter Observatory telescope (CSO) will be moved from Mauna Kea, Hawaii to Chajnantor Plateau, Chile in 2022, and renamed as Leighton Chajnantor Telescope (LCT). The altitude of the new site of LCT is 5050 m, and the average wind speed is about 10 m/s. However, the pointing accuracy of LCT will be improved to 1 arc-second (rms), and the rotating speed of LCT's antenna will be improved to 2 degrees/sec, in order to achieve its new scientific aim of large survey in the sub-millimeter waveband. More precise pointing accuracy and faster rotating speed under higher wind speed makes the servo control of LCT very challenging, because both the steady-state and the transient performances of the servo control system are required to get improved under larger disturbance, while the mechanical structure of LCT is less rigid due to the adoption of lean and optimized design. To solve this problem, in this work, a state-space model of the LCT servo control system is constructed, and the Davenport wind disturbance model for LCT is also constructed for simulating wind disturbance. To improve the stability and controllability, a robust controller of the servo system is designed based on H-infinity control theory with considering the disturbance of high wind speed. Simulation analysis verifies the capability of the designed controller for improving LCT's pointing accuracy and its antenna's rotating speed. This research is of good significance for the refurbishment of LCT and the achievement of its new scientific aim.
引用
收藏
页数:15
相关论文
共 15 条
[1]  
ALMA, 2010, CLIM COND CHAJN SIT
[2]   Revisiting the LuGre Friction Model STICK-SLIP MOTION AND RATE DEPENDENCE [J].
Astrom, Karl Johan ;
Canudas-de-wit, Carlos .
IEEE CONTROL SYSTEMS MAGAZINE, 2008, 28 (06) :101-114
[3]  
Chen JK, 2013, INT CONF INFO SCI, P73
[4]  
Control Systems Research (CSR) Inc., 1978, OP SERV MAN NC400 SE
[5]   WIND-INDUCED DYNAMICS OF A DEEP SPACE NETWORK ANTENNA [J].
GAWRONSKI, W ;
BIENKIEWICZ, B ;
HILL, RE .
JOURNAL OF SOUND AND VIBRATION, 1994, 178 (01) :67-77
[6]   Antenna control systems:: From PI to H∞ [J].
Gawronski, W .
IEEE ANTENNAS AND PROPAGATION MAGAZINE, 2001, 43 (01) :52-60
[7]  
Gawronski W., 1994, IFAC Proceedings Volumes, V27, P393, DOI [10.1016/S1474-6670(17)45831-9, DOI 10.1016/S1474-6670(17)45831-9]
[8]   Control and pointing challenges of large antennas and telescopes [J].
Gawronski, Wodek .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2007, 15 (02) :276-289
[9]  
Gawronski W, 2008, MECH ENG SER, P1, DOI 10.1007/978-0-387-78793-0_1
[10]  
Hu KY, 2014, IEEE INT CONF ELECTR, P268