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Drift Analysis in Studying the Convergence and Hitting Times of Evolutionary Algorithms: An Overview
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作者 He Jun, Yao Xin1.State Laboratory of Software Engineering, Wuhan University, Wuhan 430072, Hubei,China 2.School of Computer Science, University of Birmingham, Birmingham B15 2TT, England 《Wuhan University Journal of Natural Sciences》 CAS 2003年第S1期143-154,共12页
This paper introduces drift analysis approach in studying the convergence and hitting times of evolutionary algorithms. First the methodology of drift analysis is introduced, which links evolutionary algorithms with M... This paper introduces drift analysis approach in studying the convergence and hitting times of evolutionary algorithms. First the methodology of drift analysis is introduced, which links evolutionary algorithms with Markov chains or supermartingales. Then the drift conditions which guarantee the convergence of evolutionary algorithms are described. And next the drift conditions which are used to estimate the hitting times of evolutionary algorithms are presented. Finally an example is given to show how to analyse hitting times of EAs by drift analysis approach. 展开更多
关键词 evolutionary algorithms CONVERGENCE hitting time drift analysis
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Low-frequency Periodic Error Identification and Compensation for Star Tracker Attitude Measurement 被引量:12
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作者 WANG Jiongqi XIONG Kai ZHOU Haiyin 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2012年第4期615-621,共7页
The low-frequency periodic error of star tracker is one of the most critical problems for high-accuracy satellite attitude determination.In this paper an approach is proposed to identify and compensate the low-frequen... The low-frequency periodic error of star tracker is one of the most critical problems for high-accuracy satellite attitude determination.In this paper an approach is proposed to identify and compensate the low-frequency periodic error for star tracker in attitude measurement.The analytical expression between the estimated gyro drift and the low-frequency periodic error of star tracker is derived firstly.And then the low-frequency periodic error,which can be expressed by Fourier series,is identified by the frequency spectrum of the estimated gyro drift according to the solution of the first step.Furthermore,the compensated model of the low-frequency periodic error is established based on the identified parameters to improve the attitude determination accuracy.Finally,promising simulated experimental results demonstrate the validity and effectiveness of the proposed method.The periodic error for attitude determination is eliminated basically and the estimation precision is improved greatly. 展开更多
关键词 star trackers attitude determination low-frequency periodic error gyro drift precision analysis
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