微纳聚合体卫星的对称式重构规划算法

为解决微纳聚合体卫星变构过程中,聚合体各部分之间的动力学耦合导致的卫星整体姿态翻转或紊乱,提出了一种对称式变构规划算法。首先建立了铰链约束下的漂浮基多刚体系统动力学模型,研究了重构过程中各运动模块对本体姿态的影响,提出当每两个运动模块位置与转动方向满足对称性条件时,两者对本体姿态的影响可在一定程度上相互抵消。基于上述理论,在A*算法中引入最优分配度量和对称性判定,设计了并行对称重构规划算法。仿真结果表明,该规划算法可实现重构过程中多模块并行、对称运动,重构过程总步数较少,运动模块对本体姿态的影响小。     

矩形橡胶复合材料层合板的大变形研究

本文应用Ｋｉｒｃｈｈｏｆｆ假设和ＶｏｎＫａｒｍａｎ理论对正交各向异性的矩形橡胶复合材料层合板进行了几何非线性分析。与线性结果相比,大变形理论所得结果更具准确性。     

一个非常规前体机身的流动显示研究

描述了有类似Ｅｒｉｃｋｓｏｎ前体的非常规机身的初步流动显示研究结果,包括测力、表面油流和激光片光流动显示结果和用层流Ｎ－Ｓ方程进行数值模拟的结果。计算和试验的参数范围：α＝０°～５０°,β＝０°～２０°,虽然计算与试验所用的外形在后部有一些不同,但是两者在涡的位置方面显示了良好的一致性。同时研究也表明,大攻角的流动特性可以通过改变机身前体形状进行控制。通过研究还表明,这类前体在改善大攻角横侧方向安定性方面具有很大的潜力。     

西藏矿产开发中生态补偿费用分摊的博弈研究——基于利润分配的视角

西藏生态补偿费用分摊是西藏矿产开发生态补偿机制中的重要内容之一.由于脱胎于西方经典生态补偿理论的传统生态补偿费用分摊理论与西方生态补偿理论的异源性差异,当前我国费用分摊实践缺乏统一的方法论基础.文章以矿产相关企业间独立决策与统一决策利润博弈为主线,分析不同决策方式下相关企业的最大化利润决策行为,旨在协调矿产开采企业、冶炼加工企业与资源使用企业的关系,分析企业行为的内在逻辑和生态费用分摊的基础.     

AIRCRAFT CONCEPT EVALUATION AND EFFECTIVENESS-BASED DECISION-MAKING

Based on effectiveness analysis, a novel method is presented for combat aircraft top-hierarchy concept evaluation and decision-making. Applying multi-criterion decision-making （MCDM） and analytic hierarchy process, the new method can help to overcome the limitations of existing evaluation systems and decision-make methods. The proposed method includes the following process~ （1） Establish a multi-criterion and multi-hierarchy evaluation attribute system by introducing combat effectiveness~ （2） Assign weight to the attributes and normalize them; （3） Evaluate and decision-make top-hierarchy aircraft concept based on effectiveness to reach a satisfactory design by comprehensively applying four multi-criterion decision-making methodologies, i.e. grey correlation pro- jection method, weighted summation method, weighted quadrature method and ideal solution decision-making method, while considering the attribute hierarchy system and the logical relations among the attributes. Finally, an example is given to indicate the validity and feasibility of the proposed method.     

On-orbit determination and adjustment of electrostatic accelerometer lever arm

In order to ensure the proof mass center of electrostatic accelerometer (EA) is fixed at the center of gravity of satellite as precisely as possible, an on-orbit determination and adjustment strategy of EA lever arm is presented in this paper. The EA lever arm is determined using the observations of EA, gyro and magnetometer first. Then it is adjusted by screw slider mechanism. The simulation results demonstrate that the proposed strategy can be carried out several times to yield better accuracy. Meanwhile, the optimal geographic location for EA lever arm determination along each axis is found.     

Forming and keeping fast fly-around under constant thrust

A new switching control algorithm under constant thrust is designed for the chaser fast flying around the target spacecraft along a specified fly-around trajectory. The switching control laws are obtained based on the acceleration sequences and the on time of thrusters which can be computed by the time series analysis method. The perturbations and fuel consumptions are addressed during the computation of the on time of thrusters. Furthermore, the relative position parameters of the target spacecraft are obtained by using the vision measurement and the target fly-around positions are calculated through the isochronous interpolation method. The change of the relative position and the relative velocity of the chaser during the constant thrust fast fly-around are presented through simulation example. It is proved that, with the switching control laws, the chaser will fast fly around the target spacecraft along the specified fly-around trajectory.     

从EFA到“台风”看鸭式布局飞机设计的可持续发展

在关键技术上追求可持续发展,就要掌握好20世纪90年代国际先进技术战斗机一些有用的技术,相信凭借这些技术的支撑,鸭式布局设计必将为飞机设计的后续研究,为新世纪有人机或无人机的研发带来再创辉煌的光明前景。     

DELMIA在某民机前货舱门装配仿真中的应用

在现代自动化作业系统中,操作和管理的大多是一些复杂系统和各种数字化设备,这对操作人员观察周围环境和完成精准操作任务的要求很高。通过人机工程技术分析,可以对这些复杂、易错的任务逐个分析,合理分配注意力、安排操作顺序,既减轻操作人员的工作负荷又避免出错,切实提高人机工效。