基于非线性模型预测的翼伞系统控制研究

翼伞系统在飞行过程中,受外界不确定因素的影响呈现出非线性特性和耦合性．应用非线性模型预测控制理论对翼伞系统飞行控制进行了研究,提出基于非线性模型预测控制的翼伞系统控制律设计方法,并推导出控制律解析式．仿真研究表明,合理地选择泰勒展开级数和预测周期,通过泰勒级数展开并截尾后的翼伞非线性控制系统可以表现出良好的控制性能．     

舰艇火控系统特点分析

本文研究了舰艇火控系统公共特点,并分别对舰炮、导弹、鱼雷、深水炸弹火控系统进行了特点分析,最后引出了舰艇火控系统特点分析的两点结论。     

水面舰艇电子武备基座水平度的检验与修正

论述了舰船电子武备基座水平度的检验与修正方法,探讨了影响基座水平度变化的诸多因素及预防措施.通过建立物理模型和数学模型,提出了基座水平误差修正方法.该方法在某型导弹驱逐舰现代化改装中得到了应用,收到了良好的效果.     

公安边防部门刑事侦查权的取得与完善

公安边防部门取得刑事侦查权,是侦查体制改革的结果。但在边防管辖和查办案件的种类、边防海警刑事办案权的实现、边防检查站查获的刑事案件的管辖、公安边防部门侦查主体资格的完善等方面,还应继续改革．使边防部门刑事侦查机制不断完善。     

一种防空指令修正弹控制模式研究

针对防空指令修正弹的方案设计问题,探讨了一种通过选择弹丸在有控段某点停止控制而恰能完成修正指标的外弹道控制模式,推导了有控弹丸平均侧向速度和剩余飞行时间的估算公式,给出了最佳停控点的确定判据.对上述控制模式进行了仿真计算,得到不同修正条件下的侧偏修正量及攻角曲线.仿真结果表明,该控制模式具有较高的控制精度,侧偏修正最大误差不超过±2.5%,且在该模式下弹丸也可保持飞行稳定.该研究结果可用于指导防空指令修正弹的方案设计.     

分形理论在装备保障组织设计中的应用研究

基于分形理论,提出了一种适应敏捷化要求的分形装备保障系统组织模型,能够通过快速的重构以响应战场环境的变化。阐明了其层次性、自相似、自组织和自优化的组织结构特点,分析了其运行模式。     

Scheduling a production–distribution system to optimize the tradeoff between delivery tardiness and distribution cost

We consider a make‐to‐order production–distribution system with one supplier and one or more customers. A set of orders with due dates needs to be processed by the supplier and delivered to the customers upon completion. The supplier can process one order at a time without preemption. Each customer is at a distinct location and only orders from the same customer can be batched together for delivery. Each delivery shipment has a capacity limit and incurs a distribution cost. The problem is to find a joint schedule of order processing at the supplier and order delivery from the supplier to the customers that optimizes an objective function involving the maximum delivery tardiness and the total distribution cost. We first study the solvability of various cases of the problem by either providing an efficient algorithm or proving the intractability of the problem. We then develop a fast heuristic for the general problem. We show that the heuristic is asymptotically optimal as the number of orders goes to infinity. We also evaluate the performance of the heuristic computationally by using lower bounds obtained by a column generation approach. Our results indicate that the heuristic is capable of generating near optimal solutions quickly. Finally, we study the value of production–distribution integration by comparing our integrated approach with two sequential approaches where scheduling decisions for order processing are made first, followed by order delivery decisions, with no or only partial integration of the two decisions. We show that in many cases, the integrated approach performs significantly better than the sequential approaches. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005     

A novel variable topology design for a multi-flexible ejection mechanism

The airborne missile launch mechanism often subjects to significant deformations induced by the large ejection force during high-speed actuations in missile ejection process, leading to a substantial deviation of separation parameters from designed values that threats safety of the carrier. This study proposes a novel variable topology design for launch mechanism, achieved via a Prismatic-Revolute-Revolute pair (PR-R) motion formed by the structural gap with a specific direction. It enables launch mechanism variability during missile ejection process and optimizes the ejection force given by the front and back ejection arms, and greatly optimizes the separation parameters during missile ejection. The kinetics simulation analysis is conducted under working conditions of the original ejection mechanism and the novel mechanism with variable topology design, respectively. The results show that the novel variable topology design is more befitting for the launch process in terms of system safety and controllability, effectively improving the separation posture, restraining the flexible effect of the mechanism, and fulfilling the effectiveness of the design value of multi-rigid body.     

越肩发射的两种方式

首先介绍了越肩发射的两种发射方式及其原理,然后对这两种方式的性能优劣进行了详细的比较和分析,最后讨论了越肩发射与以往攻击方式的不同和对未来空战所产生的影响及其应用情况,并得出了一些有益的结论。     

风场的科学计算可视化在导弹射击中的应用

在导弹射击时,消除风会对导弹飞行造成不利的影响,因此基于可视化分析的研究模型、流程等,利用科学计算方法直观分析优点对风的大小和方向进行分析,并采用开放图形接口对实验风场数据进行了三维图形绘制以提高导弹打击目标的精度,对实际中导弹的风场阻力研究有一定的指导意义.