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	Comprehensive SNN Compression Using ADMM Optimization and Activity Regularization 期刊论文 OAI收割 IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2021, 页码: 15 作者: Deng, Lei; Wu, Yujie; Hu, Yifan; Liang, Ling; Li, Guoqi \| 收藏 \| 浏览/下载：38/0 \| 提交时间：2022/06/21 Neurons Computational modeling Quantization (signal) Optimization Encoding Task analysis Synapses Activity regularization alternating direction method of multiplier (ADMM) connection pruning spiking neural network (SNN) compression weight quantization
	Nash Equilibrium Computation in Subnetwork Zero-Sum Games With Switching Communications 期刊论文 OAI收割 IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2016, 卷号: 61, 期号: 10, 页码: 2920-2935 作者: Lou, Youcheng; Hong, Yiguang; Xie, Lihua; Shi, Guodong \| 收藏 \| 浏览/下载：32/0 \| 提交时间：2018/07/30 Heterogeneous stepsizes joint connection multi-agent systems Nash equilibrium weight-unbalanced graphs
	An optimizing BP neural network algorithm based on genetic algorithm 期刊论文 OAI收割 ARTIFICIAL INTELLIGENCE REVIEW, 2011, 卷号: 36, 期号: 2, 页码: 153-162 作者: Ding, Shifei; Su, Chunyang; Yu, Junzhao \| 收藏 \| 浏览/下载：23/0 \| 提交时间：2019/12/16 Genetic algorithm (GA) BP neural network Connection weight UCI data
	Structure optimization of strap-down inertial navigation system support (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China 作者: Wang J.; Sun H.; Sun H. 收藏 \| 浏览/下载：31/0 \| 提交时间：2013/03/25 In order to meet the requirement of inertial navigation components and minimizing the system's weight and topological optimization was conducted. Then topological optimization and size optimization were conducted under conditions of random vibration and impact. Firstly according to the dynamic characteristics of missile and requirement of inertial navigation system the structure of inertial navigation support was designed according to types of missile connection and space arrangement of electronic components the method of transforming multi-loading cases to multi-loading constraints was used to optimizing the size of the support under conditions of random vibration and impact. Comparing to the original support structures RMS accelerations in installed points reduced by 25.2% under random vibration the weight of optimal structures reduced by 28.1% the structures also met the requirement of inertial navigation system under condition of impact. The support structure shows improvements in both dynamic characteristic and light weight comparing with the original one. 2011 IEEE.
	Optimal design of strap-down inertial navigation support under random loads (EI CONFERENCE) 会议论文 OAI收割 2010 IEEE International Conference on Information and Automation, ICIA 2010, June 20, 2010 - June 23, 2010, Harbin, Heilongjiang, China 作者: Li M. 收藏 \| 浏览/下载：29/0 \| 提交时间：2013/03/25 In order to realize miniaturization and light weight of the strap-down inertial navigation system and then to make sure that it works well under random loads optimal design is applied to the strap-down inertial navigation support with the methods of topology optimization and size optimization. Firstly based on the installation requirement of devices and connection requirement of the support and the carrier the initial structure of the support is designed. Topology optimization with FEA software ANSYS is adopted on the initial structure to get the basic one. Then 5 critical sizes are chosen as design variables and the support structure is optimized by means of size optimization to reach light weight with satisfying the requirement of dynamic stiffness. Finally random vibration analysis is applied to the initial structure. In the mean time random vibration test is carried out to qualify the analysis method. After the qualification a random vibration analysis is applied to the optimized support structure to get the rms of displacement response and acceleration response of the support to validate whether the optimized structure is appropriate. The results indicate that the dynamic stiffness of the optimized support structure satisfies the design requirements and its weight is lighter 49.38% than that of the initial one. This research can be a reference to the structure design of supports under random loads and the result has been applied to the development and manufacture of a prototype aerocraft. 2010 IEEE.