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91.
用人工神经网络BP算法评价城市火灾风险 总被引:2,自引:0,他引:2
吴立志 《中国人民武装警察部队学院学报》2001,17(3):30-32
深入讨论了人工神经网络的BP算法在城市火灾风险评价中应用的可行性和一些具体做法. 相似文献
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93.
基于路径规划的无人机飞行冲突解脱技术 总被引:1,自引:0,他引:1
在无人机与有人机共用空域时,随时可能发生飞行冲突,应当有一种可靠的冲突解脱技术,保证无人机的空域运行安全。为此,构建了基于正三角形栅格法的空域运行环境,改进了以往十字栅格环境规划动态路径的缺陷;提出了基于空间分割的改进蚁群算法,提高了算法的寻优性能与路径规划能力。最后结合ADS-B系统的工作原理,在利用卡尔曼滤波对ADS-B信息进行修正的基础上,设计了无人机冲突感知的技术方案,并用实时的路径重规划技术实现飞行冲突的解脱。最终的仿真实验验证了飞行冲突解脱技术方案的有效性,可为未来无人机的空域运行技术提供一定的理论参考。 相似文献
94.
介绍了蚁群算法的原理,然后对现有蚁群算法进行了一些改进,使它能够快速地收敛以满足高速变化的卫星网络拓扑结构.采用改进的虚拟拓扑策略解决了卫星网络拓扑高速变换的问题,将改进的蚁群算法应用于其上,并给出了相应的性能评估.所提出的改进的虚拟拓扑策略,能够大大减少一个系统周期内卫星网的时间片个数.应用于此基础上的改进的蚁群算法也体现了较好的性能. 相似文献
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96.
In order to improve the infrared detection and discrimination ability of the smart munition to the dy-namic armor target under the complex background, the multi-line array infrared detection system is established based on the combination of the single unit infrared detector. The surface dimension features of ground armored targets are identified by size calculating solution algorithm. The signal response value and the value of size calculating are identified by the method of fuzzy recognition to make the fuzzy classification judgment for armored target. According to the characteristics of the target signal, a custom threshold de-noising function is proposed to solve the problem of signal preprocessing. The multi-line array infrared detection can complete the scanning detection in a large area in a short time with the characteristics of smart munition in the steady-state scanning stage. The method solves the disadvan-tages of wide scanning interval and low detection probability of single unit infrared detection. By reducing the scanning interval, the number of random rendezvous in the infrared feature area of the upper surface is increased, the accuracy of the size calculating is guaranteed. The experiments results show that in the fuzzy recognition method, the size calculating is introduced as the feature operator, which can improve the recognition ability of the ground armor target with different shape size. 相似文献
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99.
This paper presents an actuator used for the trajectory correction fuze, which is subject to high impact loadings during launch. A simulation method is carried out to obtain the peak-peak stress value of each component, from which the ball bearings are possible failures according to the results. Subsequently, three schemes against impact loadings, full-element deep groove ball bearing and integrated raceway, needle roller thrust bearing assembly, and gaskets are utilized for redesigning the actuator to effectively reduce the bearings' stress. However, multi-objectives optimization still needs to be conducted for the gaskets to decrease the stress value further to the yield stress. Four gasket's structure parameters and three bearings' peak-peak stress are served as the four optimization variables and three objectives, respectively. Optimized Latin hypercube design is used for generating sample points, and Kriging model selected according to estimation result can establish the relationship between the variables and objec-tives, representing the simulation which is time-consuming. Accordingly, two optimization algorithms work out the Pareto solutions, from which the best solutions are selected, and verified by the simulation to determine the gaskets optimized structure parameters. It can be concluded that the simulation and optimization method based on these components is effective and efficient. 相似文献
100.
Muhammad Imran Dong-yan Shi Li-li Tong Ahsan Elahi Hafiz Muhammad Waqas Muqeem Uddin 《防务技术》2021,17(4):1190-1206
This paper presents the design optimization of composite submersible cylindrical pressure hull subjected to 3 MPa hydrostatic pressure. The design optimization study is conducted for cross-ply layups [0s/90t/0u], [0s/90t/0u]s, [0s/90t]s and [90s/0t]s considering three uni-directional composites, i.e. Carbon/Epoxy, Glass/Epoxy, and Boron/Epoxy. The optimization study is performed by coupling a Multi-Objective Genetic Algorithm (MOGA) and Analytical Analysis. Minimizing the buoyancy factor and maximizing the buckling load factor are considered as the objectives of the optimization study. The objectives of the optimization are achieved under constraints on the Tsai-Wu, Tsai-Hill and Maximum Stress composite failure criteria and on buckling load factor. To verify the optimization approach, optimization of one particular layup configuration is also conducted in ANSYS with the same objectives and constraints. 相似文献