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Nearest neighbor vector analysis of SDSS DR5 galaxy distribution
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作者 Yongfeng Wu Weike Xiao +2 位作者 rongjun mu David Batuski Andre Khalil 《Natural Science》 2013年第1期47-51,共5页
We present the nearest neighbor distance (NND) analysis of SDSS DR5 galaxies. We give NND results for observed, mock and random sample, and discuss the differences. We find the observed sample gives us a significantly... We present the nearest neighbor distance (NND) analysis of SDSS DR5 galaxies. We give NND results for observed, mock and random sample, and discuss the differences. We find the observed sample gives us a significantly stronger aggregation characteristic than the random samples. Moreover, we investigate the direction of NND and find the direction has close relation with the size of the NND for the observed sample. 展开更多
关键词 Nearest NEIGHBOR Distance Nearest NEIGHBOR Vector ANISOTROPY SDSS DR5 GALAXY DISTRIBUTION
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Neural network based adaptive nonsingular practical predefined-time fault-tolerant control for hypersonic morphing aircraft
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作者 Shihao XU Changzhu WEI +1 位作者 Litao ZHANG rongjun mu 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第4期421-435,共15页
This paper develops a novel Neural Network(NN)-based adaptive nonsingular practical predefined-time controller for the hypersonic morphing aircraft subject to actuator faults. Firstly, a novel Lyapunov criterion of pr... This paper develops a novel Neural Network(NN)-based adaptive nonsingular practical predefined-time controller for the hypersonic morphing aircraft subject to actuator faults. Firstly, a novel Lyapunov criterion of practical predefined-time stability is established. Following the proposed criterion, a tangent function based nonsingular predefined-time sliding manifold and the control strategy are developed. Secondly, the radial basis function NN with a low-complexity adaptation mechanism is incorporated into the controller to tackle the actuator faults and uncertainties. Thirdly, rigorous theoretical proof reveals that the attitude tracking errors can converge to a small region around the origin within a predefined time, while all signals in the closed-loop system remain bounded. Finally, numerical simulation results are presented to verify the effectiveness and improved performance of the proposed control scheme. 展开更多
关键词 Hypersonic morphing aircraft(HMA) Neural network(NN) Adaptive control Practical predefined-time control Fault-tolerant control
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