太阳辐射对ER3BP拉格朗日点的影响

为了研究Halo轨道中继通信以及行星际轨道转移等问题,需要首先对拉格朗日点(平动点)的理论进行分析。使用考虑太阳辐射的椭圆型限制性三体建模,代替原有的圆型限制性三体建模,提高了建模的精度。提出了在L1,L2,L3点的更为精确的新解析解,经过Matlab仿真,其相对于精确数值解的误差,分别为Ammar的解析解的13.13%,29.51%,0.46%。     

地面等待模型中的旅客延误时间成本分析与仿真

针对多机场地面等待问题MAGHP(Multi Airport Ground Holding Problem),深入研究了影响旅客延误时间的因素,并将其应用于数学模型中目标函数的计算。将航班延误时间转化为旅客延误时间,提出了一个在航班取消情况下减少旅客延误的新方法,并与多机场地面等待模型进行了比较,仿真结果表明,可以大幅度减少旅客延误时间。     

对称矩阵反问题解的稳定性

考虑如下对称矩阵反问题：问题Ⅰ：给定Ｘ,Ｂ∈Ｒ（ｎ×ｎ）,求Ａ∈ＳＲ（ｎ×ｎ）使得ＡＸ＝Ｂ,其中ＳＲ（ｎ×ｎ）＝｛｛Ａ｜Ａ∈Ｒ（ｎ×ｎ）,ＡＴ＝Ａ｝。问题Ⅱ：给定,求使得其中是矩阵的Ｆｒｏｂｅｎｉｕｓ范数,ＳＡ表示问题Ⅰ的解集合。本文讨论问题Ⅰ解的稳定性,给出问题Ⅱ解的扰动界。     

AFM电场诱导氧化加工技术制备微纳米结构

大气状态下利用接触模式原子力显微镜(AFM)动态电场和静态电场及轻敲模式AFM静态电场制备了一维纳米光栅,对纳米光栅结构的特征进行了比较并对电场诱导阳极氧化加工的机理作了相应的理论分析。     

Resonant quasi-periodic near-rectilinear Halo orbits in the Elliptic-Circular Earth-Moon-Sun Problem

Motivated by the near-future re-exploration of the cislunar space, this paper investigates dynamical substitutes of the Earth-Moon’s resonant Near-Rectilinear Halo Orbits (NRHOs) under the Elliptic-Circular Restricted Four-Body Problem formulation of the Earth-Moon-Sun system. This model considers that the Earth and Moon move in elliptical orbits about each other and that a third body, the Sun, moves in a circular orbit about the Earth-Moon barycenter. By making use of this higher-fidelity dynamical model, we are able to incorporate the Sun’s influence and the Moon’s eccentricity, two of the most significant perturbations of the cislunar environment. As a result of these perturbations, resonant periodic NRHOs of the Earth-Moon Circular Restricted Three-Body Problem (CR3BP) are hereby replaced by two-dimensional quasi-periodic tori that better represent the dynamical evolution of satellites near the vicinity of the Moon. We present the steps and algorithms needed to compute these dynamical structures in the Elliptic-Circular model and subsequently assess their utility for spacecraft missions. We focus on the planned orbit for the NASA-led Lunar Gateway mission, a 9:2 synodic resonant L₂ southern NRHO, as well as on the 4:1 synodic and 4:1 sidereal resonances, due to the proximity to the nominal orbit and their advantageous dynamical properties. We verify that the dynamical equivalents of these orbits preserve key dynamical attributes such as eclipse avoidance and near-linear stability. Furthermore, we find that the higher dimensionality of quasi-periodic solutions offers interesting alternatives to mission designers in terms of phasing maneuvers and low-altitude scientific observations.     

应用于传感器网络覆盖问题的能量有效性启发式机制

提出了一种解决无线传感器网络覆盖问题的分布式启发式机制。该机制在节能前提下,得到优化的目标覆盖集合,以实现对目标监控区域的完全覆盖,并通过对其中重点目标集合的冗余覆盖来满足对重点目标集的可靠监控。同时,该目标覆盖集合与数据汇集点在通信结构上保持连通性。本文采用了改进的蚁群优化算法（最大最小蚁群混合算法）来实现上述启发式机制。通过构造新颖的启发式因子,人工蚂蚁能够由局域信息感知传感器网络的能量状况和覆盖能力,从而自适应地建立具备通信连通性的数据汇集路径。此外,将信息素浓度调节因子和评价函数引入了信息素更新规则的设计,使得蚁群在扩大搜索范围的基础上,提高了解的质量,且避免了求解过程陷入局部最优。算法的输出为能量有效的优化解集,具备较长生命周期,能够在保证与数据汇集点可靠连通的同时实现对目标区域的有效覆盖。     

点接触圆柱蜗杆传动的设计原理

本文在对蜗轮副啮合原理分析的基础上,通过在共轭齿面上预先设置啮合位置,详细推导了失配齿面的几何参数和接触特性的计算公式,论述了点接触圆柱蜗杆传动的设计原理。应用本文的原理,采用优化综合的方法,可以使圆柱蜗杆传动直接实现点接触和完全互换,并具有良好的接触特性,使对误差的敏感性降低,缩短装配中的辅助时间,且传动质量得到改善。     

Effect of Variable Selection on Multidisciplinary Design Optimization： a Flight Vehicle Example

Different multidisciplinary design optimization (MDO) problems are formulated and compared. Two MDO formulations are applied to a sounding rocket in order to optimize the performance of the rocket. In the MDO of the referred vehicle, three disciplines have been considered,which are trajectory, propulsion and aerodynamics. A special design structure matrix is developed to assist data exchange between disciplines. This design process uses response surface method (RSM) for multidisciplinary optimization of the rocket. The RSM is applied to the design in two categories: the propulsion model and the system level. In the propulsion model, RSM deter-mines an approximate mathematical model of the engine output parameters as a function of design variables. In the system level, RSM fits a surface of objective function versus design variables. In the first MDO problem formulation, two design variables are selected to form propulsion discipline. In the second one, three new design variables from geometry are added and finally, an optimization method is applied to the response surface in the system level in order to find the best result. Application of the first developed multidisciplinary design optimization procedure increased accessible altitude (performance index) of the referred sounding rocket by twenty five percents and the second one twenty nine.     

振动对电连接器接触性能退化的影响

长期振动作用下,电连接器插孔易出现应力松弛现象,引起接触性能的退化。针对接触件的结构特点,提出了一种接触压力监测方法和接触性能退化试验方案,设计了试验电路并进行了试验。试验结果表明:(1)接触压力波动程度受振动频率与加速度共同影响,高频振动下,接触压力值波动程度约为低频振动下的3~7倍;但随着振动加速度的增大,低频振动下接触压力波动程度的增幅更为明显;(2)随着振动次数的增加,接触压力逐渐减小;振幅越大,接触压力的降幅越明显;试验后插孔槽宽的变化规律与之吻合,且振幅越大,振动累积效应的差异性越明显;但接触电阻无明显的变化趋势。因此,振动引发的插孔应力松弛现象和电连接器接触性能退化的演变极其缓慢,但振动影响的差异性可能会导致突发性偶然失效现象。