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371.
本文探讨了市场经济下的消防管理监督机制的设计,用博弃理论构造了一个消防管理监督模型。提出了新时期消防管理监督应以防火检查和经济惩罚相结合的监管机制。 相似文献
372.
本文运用二维约化摄动方法首次导出磁层顶边界区剪切流的非线性波动方程,并对其非线性性态作了一些定性讨论。 相似文献
373.
原亮 《军械工程学院学报》1991,(4)
本文针对使用8088汇编语言实现基2FFT 的难点,就旋转因子的求取、比例系数的选择、16位乘积的获得以及运算溢出等问题提出了有效的解决方法,并给出了具体程序.从而,可使 FFT 运算速度较单纯运行相应的高级语言程序提高20倍左右. 相似文献
374.
梁前超 《海军工程大学学报》1990,(2)
在各种复杂的分支传动扭振系统中,由于计算工作量大而对计算机内存及速度提出了一定的要求。本文比较了三种常用的计算扭振固有频率的方法(霍尔茨法、传递矩阵法和直接法),认为采用基于传递矩阵的直接法计算更简单、明了。因其不需要求解结点方程,故不会产生前两种方法中出现的方程奇异性问题。文中结合一个前后分叉的七分支系统,介绍了直接法的实际运用。 相似文献
375.
376.
运用H_∞理论设计摄动模型的控制器 总被引:1,自引:0,他引:1
利用MATLAB软件包及Robust-ControlToolbox对柴油机带水力测功器系统进行了H∞鲁棒控制器的设计研究,介绍了设计方法、设计过程和设计结果,并对设计控制器进行了仿真分析. 相似文献
377.
为了实施饱和攻击,需要对撞击角度与飞行时间同时进行控制。通过一种导弹撞击角度与飞行时间两阶段控制制导策略实现导弹撞击角度与飞行时间控制。第一阶段:基于切换滑模思想在纵向通道内对导弹飞行时间进行精确控制,侧向通道制导指令采用传统的纯比例导引律。第二阶段:切换到含重力补偿轨迹调节最优制导律对撞击角度进行精确控制,与显式制导不同,该制导律显式包含重力补偿项。设计数值仿真验证撞击角度与飞行时间两阶段控制制导方法的有效性,仿真结果表明,所给出的撞击角度与飞行时间两阶段控制制导方法能够实现撞击角度与飞行时间的同时控制。 相似文献
378.
Tracking maneuvering target in real time autonomously and accurately in an uncertain environment is one of the challenging missions for unmanned aerial vehicles(UAVs).In this paper,aiming to address the control problem of maneuvering target tracking and obstacle avoidance,an online path planning approach for UAV is developed based on deep reinforcement learning.Through end-to-end learning powered by neural networks,the proposed approach can achieve the perception of the environment and continuous motion output control.This proposed approach includes:(1)A deep deterministic policy gradient(DDPG)-based control framework to provide learning and autonomous decision-making capa-bility for UAVs;(2)An improved method named MN-DDPG for introducing a type of mixed noises to assist UAV with exploring stochastic strategies for online optimal planning;and(3)An algorithm of task-decomposition and pre-training for efficient transfer learning to improve the generalization capability of UAV's control model built based on MN-DDPG.The experimental simulation results have verified that the proposed approach can achieve good self-adaptive adjustment of UAV's flight attitude in the tasks of maneuvering target tracking with a significant improvement in generalization capability and training efficiency of UAV tracking controller in uncertain environments. 相似文献
379.
In this paper, based on a bidirectional parallel multi-branch feature pyramid network (BPMFPN), a novel one-stage object detector called BPMFPN Det is proposed for real-time detection of ground multi-scale targets by swarm unmanned aerial vehicles (UAVs). First, the bidirectional parallel multi-branch convolution modules are used to construct the feature pyramid to enhance the feature expression abilities of different scale feature layers. Next, the feature pyramid is integrated into the single-stage object detection framework to ensure real-time performance. In order to validate the effectiveness of the proposed algorithm, experiments are conducted on four datasets. For the PASCAL VOC dataset, the proposed algorithm achieves the mean average precision (mAP) of 85.4 on the VOC 2007 test set. With regard to the detection in optical remote sensing (DIOR) dataset, the proposed algorithm achieves 73.9 mAP. For vehicle detection in aerial imagery (VEDAI) dataset, the detection accuracy of small land vehicle (slv) targets reaches 97.4 mAP. For unmanned aerial vehicle detection and tracking (UAVDT) dataset, the proposed BPMFPN Det achieves the mAP of 48.75. Compared with the previous state-of-the-art methods, the results obtained by the proposed algorithm are more competitive. The experimental results demonstrate that the proposed algorithm can effectively solve the problem of real-time detection of ground multi-scale targets in aerial images of swarm UAVs. 相似文献
380.
Shu-jie Liu Bi-dong Wu Jia-ni Xie Zhi-min Li Chong-wei An Jing-yu Wang Xiao-dong Li 《防务技术》2021,17(5):1775-1781
Insensitive energetic materials are promising in the defense weapons field. However, energetic materials still suffer from great challenges and the concern about their safety limits their utilization. In this work, insensitive energetic explosive 3,3′-diamino-4,4′-azoxyfurazan/hexahydro-1,3,5-trinitro-1,3,5-triazine (DAAF/RDX) microspheres were fabricated by self-assembly method. Rod-like DAAF/RDX was prepared by mechanical ball milling for comparison. DAAF/RDX composites with different mass ratios (90:10, 80:20, and 70:30) were obtained. The morphologies and structures of as-obtained DAAF/RDX composites were characterized by scanning electron microscopy (SEM), powder x-ray diffraction (PXRD) and fourier transform infrared spectroscopy (FT-IR). The results showed that DAAF/RDX microspheres exhibited regular shaped microspheres with sizes from 0.5 to 1.2 μm. There was no crystal transition during the modification process. The thermal properties of as-obtained materials were then evaluated by differential scanning calorimetry (DSC) and materials studio software. DAAF/RDX microspheres showed an advanced decomposition peak temperature compared with rod-like DAAF/RDX. The binding energy and peak temperature values at zero βi (TP0) of DAAF/RDX (90:10) increased by 36.77 kJ/mol, 1.6 °C, and 58.11 kJ/mol, 12.3 °C compared to DAAF/RDX (80:20) and DAAF/RDX (70:30), indicating the better thermal stability of DAAF/RDX (90:10). The characteristic drop height (H50) of DAAF/RDX (higher than 100 cm) composites was higher than that of raw RDX (25 cm), suggesting significant improvements in mechanical safety. The preparation of DAAF/RDX microspheres is promising for the desensitization of RDX and useful for the formation of other materials and future wide applications. 相似文献