基于RTX的实时测控系统软件设计

从无人机半物理仿真试验的整体结构出发,针对实时测控系统的需求,采用了一种较为新颖的Windows+RTX实时性方案,完成了无人机半物理仿真试验中实时测控系统的研制.既满足了试验的实时性要求,又具有很好的用户交互特性,对测控技术的发展及其在国防科技等相关领域中的应用均有重要的参考价值.     

均匀设计在柴油无灰节能降污添加剂配方研制中的应用

基于低压氧弹燃烧法研究了充氧压力分别为0．6MPa和0．9MPa时两种无灰型柴油添加剂不同配比对助燃性能的影响。采用均匀实验设计和Matlab回归优化的方法,得到复配体系的最优配方,并对其进行了验证。结果表明,由Matlab回归分析得到的完全二次回归模型最理想,0．6MPa时由该模型得到的最优配方为：添加剂A和B的质量分数分别是0．300‰和0．700‰,并通过实验验证得到的发热量达到最大,变化率为8．697％。0．9MPa时,结合直观分析和回归分析,得到与实际相符的最优配方：添加剂A和B的质量分数分别是0．600‰和0．900‰,此时发热量皮化率为4．453％。     

浅析储油罐安全容量的确定计算

由于油料具有热膨胀性,在运输和储存期间,如果油罐装油超过安全容量,当温度升高时,罐内油料体积膨胀,就可能导致溢油事故的发生,不仅造成油料数量的损失,甚至会引发火灾事故。正确确定不同油罐的安全容量,对油料的安全具有重要意义。文章阐述了油罐安全容量的概念,分析了安全容量计算不准确可能造成的危害,提出了油罐安全容量的计算方法。     

导航精度对某型电视制导无人攻击机攻击性能影响

针对电视制导无人机的作战使用方式,分析了影响其攻击性能的因素;建立了导航精度与攻击无人机捕获目标概率之间的关系;基于捷联惯导的误差分析,对无人机中制导末段的导航精度进行了计算。构建了对无人攻击机目标捕获概率进行仿真计算的方案,建立了方案航迹,对其进行了中制导精度分析和目标捕获概率计算,结果表明导航精度和捕获概率直接相关。     

Dynamic institutionalization: the foundations of Japan’s radioactive problem

Many have suggested that the true purpose behind Japan’s development of a closed nuclear-fuel cycle is to maintain the technical potential to develop nuclear weapons. However, closer examination of the development of Japan’s nuclear industry shows that, although Japan possesses advanced nuclear technologies, there has been no deliberate strategy to create a nuclear-weapon option. There is no “nuclear hedge.” To illustrate this point, this article presents a framework called “dynamic institutionalization” to explain the origins of Japan’s nuclear policies and the different sets of institutionalized pressures and constraints that have perpetuated these policies over time. Japan’s continued development of closed fuel-cycle technologies is primarily driven by domestic politics and the lack of a permanent spent-fuel management solution. On the other hand, Japan’s institutionalized nuclear forbearance is driven by the calculation that, as long as US extended deterrence remains credible, Japan’s security is best guaranteed through reliance on the US nuclear umbrella. By analytically untangling the policy of closed fuel-cycle development from the rationale for nuclear forbearance, this article provides a more nuanced view of the relationships between the domestic and international variables shaping Japan’s nuclear policies.     

A generic model of motor‐carrier fuel optimization

Fuel optimizers are decision models (software products) that are increasingly recognized as effective fuel management tools by U.S. truckload carriers. Using the latest price data of every truck stop, these models calculate the optimal fueling schedule for each route that indicates: (i) which truck stop(s) to use, and (ii) how much fuel to buy at the chosen truck stop(s) to minimize the refueling cost. In the current form, however, these models minimize only the fuel cost, and ignore or underestimate other costs that are affected by the models' decision variables. On the basis of the interviews with carrier managers, truck drivers, and fuel‐optimizer vendors, this article proposes a comprehensive model of motor‐carrier fuel optimization that considers all of the costs that are affected by the model's decision variables. Simulation results imply that the proposed model not only attains lower vehicle operating costs than the commercial fuel optimizers, but also gives solutions that are more desirable from the drivers' viewpoint. © 2008 Wiley Periodicals, Inc. Naval Research Logistics, 2008     

基于聚类算法的多无人机系统任务分配

针对现有任务分配方法在任务点较多时不易解算,且计算量大的问题,提出了基于模糊C-均值聚类算法的多无人机系统任务分配方法.首先,利用模糊C-均值聚类算法得到的隶属度矩阵对任务点进行初始分配;其次,针对基于空间划分聚类可能造成各UAV任务不均衡的问题,设计任务的局部优化调整规则;最后,结合单旅行商问题,利用Tabu Sea...     

任务分配问题的对称群方法

探讨了无人飞行器(UAV)编队的任务分配问题。任务分配是UAV协同控制的基础,其解是任务区域内各任务的一个排列。求解UAV任务分配问题的有效方法是能在合理的计算时间内找到近似最优解的启发式算法。用对称群描述UAV任务分配的搜索空间,基于右乘运算构造搜索邻域。仿真结果验证了群论禁忌搜索算法的有效性。     

航拍图像车辆检测中的圆形滤波器HOG特征快速计算

航拍图像中车辆一般近似为矩形结构,因此通过统计检测窗口中的梯度方向直方图并根据梯度主方向估计车辆朝向,将检测窗口旋转到相应方向进行分类器判别。车辆检测采用级联boosting分类器和梯度方向直方图特征,针对旋转窗口中梯度方向直方图特征的计算,设计一种基于圆形滤波器的梯度方向直方图特征。与传统基于积分直方图的梯度方向直方图特征提取方法相比,显著提高了旋转窗口中梯度方向直方图特征的计算效率,在计算每个像素的梯度时采用查找表代替梯度向量的求模和角度计算也减小了计算量。使用真实图像进行的实验表明,该车辆检测算法快速高效。     

基于响应面与遗传算法的柴油机喷射参数优化

为解决燃油喷射系统参数优化中高效寻求全局最优解问题,综合响应面设计和遗传算法的优点和不足,采用多项式响应面模型代替原始遗传算法中计算量庞大的目标特性分析模型,建立了多项式响应面模型和遗传算法相结合的参数优化方法。结合非线性规划的凸性分析证明了遗传算法在预定优化区间内全局最优解的唯一性。对优化匹配后的喷射参数进行了模拟计算,结果表明:优化后柴油机油耗降低了1.96g/(kW·h),功率上升了0.99%,排气温度降低了21.86℃。表明该方法具有简单可靠、优化效率高等特点。