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Analysis on Source Process of Strong Earthquakes in Qinghai Province Based on Broadband Data
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作者 Gao Yuan, Wu Zhongliang, and Zhou HuilanGraduate School of USTC, Academia Sinica, Beijing 100039, ChinaCenter for Analysis and Prediction, China Seismological Bureau, Beijing 100036, ChinaInstitute of Geophysics, China Seismological Bureau, Beijing 100081, China 《Earthquake Research in China》 1998年第3期17-23,共7页
Four earthquakes with M 】 6.0 occurred in Qinghai Province, China froth 1988 to 1990. Using broadband data from GDSN, the source ruptures of these earthquakes and tectonic surroundings were studied using waveform mod... Four earthquakes with M 】 6.0 occurred in Qinghai Province, China froth 1988 to 1990. Using broadband data from GDSN, the source ruptures of these earthquakes and tectonic surroundings were studied using waveform modelling combined with background data of geological tectonics. Through the analysis of apparent source time function (aSTF) and apparent time difference (aTD), the complexity of sources was discussed, and in view of source analysis, the result further supports the conclusion that the compressive stress axis of tectonic stress field in northeastern Qinghai-Xizang (Tibetan) plateau is at the NE direction, is nearly horizontal, turns counter-clockwise to the NEE or N to S direction, and is nearly horizontal close to the northern Qinghai-Xizang plateau. 展开更多
关键词 QINGHAI-XIZANG (Tibetan) plateau SOURCE process RUPTURE APPARENT SOURCE TIME function (aSTF) APPARENT TIME difference (aTD).
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μ-Synthesis control with reference model for aeropropulsion system test facility under dynamic coupling and uncertainty
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作者 Jiashuai LIU Xi WANG +4 位作者 Xi LIU Meiyin ZHU Xitong PEI Song ZHANG Zhihong DAN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2023年第10期246-261,共16页
Due to the dynamic coupling and multi-source uncertainties,it is difficult to accurately control the pressure and temperature of the Aeropropulsion System Test Facility(ASTF)in the presence of rapid command and large ... Due to the dynamic coupling and multi-source uncertainties,it is difficult to accurately control the pressure and temperature of the Aeropropulsion System Test Facility(ASTF)in the presence of rapid command and large disturbance.This paper presents the design ofμ-synthesis control to solve the problem.By incorporating the pressure ratio into the linear equation of the control valve,the modeling error of ASTF in the low frequency range is effectively reduced.Then,an uncertain model is established by considering various factors,including parameter variations,modeling error in the low frequency range,unmodeled dynamics,and changes in the working point.To address the dynamic coupling,a diagonal reference model with desired performance is incorporated intoμ-synthesis.Furthermore,all weighting functions are designed according to the performance requirements.Finally,theμ-controller is obtained by using the standardμ-synthesis method.Simulation results indicate that theμ-controller decouples the pressure and temperature dynamics of ASTF.Compared with the multivariable PI controller,integral-μcontroller,and double integral-μcontroller,the proposedμ-controller can achieve higher transient accuracy and better disturbance rejection.Moreover,the robustness of theμ-controller is demonstrated by Monte Carlo simulations. 展开更多
关键词 Aeropropulsion System Test Facility(ASTF) DECOUPLING ROBUSTNESS μ-Synthesis UNCERTAINTY
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