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Identification of vibration loads on hydro generator by using hybrid genetic algorithm 被引量:6
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作者 Shouju Li Yingxi Liu 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2006年第6期603-610,共8页
Vibration dynamic characteristics have been a major issue in the modeling and mechanical analysis of large hydro generators. An algorithm is developed for identifying vibration dynamic characteristics by means of hybr... Vibration dynamic characteristics have been a major issue in the modeling and mechanical analysis of large hydro generators. An algorithm is developed for identifying vibration dynamic characteristics by means of hybrid genetic algorithm. From the measured dynamic responses of a hydro generator, an appropriate estimation algorithm is needed to identify the loading parameters, including the main frequencies and amplitudes of vibrating forces. In order to identify parameters in an efficient and robust manner, an optimization method is proposed that combines genetic algorithm with simulated annealing and elitist strategy. The hybrid genetic algorithm is then used to tackle an ill-posed problem of parameter identification, in which the effectiveness of the proposed optimization method is confirmed by its comparison with actual observation data. 展开更多
关键词 Hybrid genetic algorithm parameteridentification Vibration responses Fieldmeasurement Simulated annealing
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IDENTIFICATION OF NONLINEAR PROPERTIES OF AN AIRCRAFT LANDING GEAR SHOCK STRUT
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作者 Zhang Zengchang Zhang Jiangjan(Institute of Vibrationn Engineering Research, Nanjing University of Aeronautics andAstronautics Nanjing , China . 210016) Wang Yuchang(Chinese Flignt Test Establishmennt , Xi’an, China 710089) 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1994年第3期188-194,共7页
A simple but realistic method for identifying nonlinear stiffness and damp-ing of an air-oil shock strut widely used in aircraft is developed.In the method a powerseries expansion is used to niodel the nonlinear dynam... A simple but realistic method for identifying nonlinear stiffness and damp-ing of an air-oil shock strut widely used in aircraft is developed.In the method a powerseries expansion is used to niodel the nonlinear dynamic properties of the strut. and after introducing new variables lhe nonlinear identitication problem can be reduced to alinear one with unknown linear paranieters. An unbiased, efficient and consistentestimator for the vector of the linear parameters is obtained under conditions of mini-mizing the sum of squared residuals which is assumed to be stationary and uncorrelatedwith the observed data.The order and the most effective independent variables in themodel are detennined by the criterion of residual series correlation infonnation entropyand the procedure of best subset regression, respectively. Experiinent demonstrates thatthe results are quite satisfactory, and the method developed is realistic, which can beused to study the dynamic properties of a strut in full detail. 展开更多
关键词 landing gear shock absorbers nonlinear system PROPERTIES parameteridentification
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