MOS电容型微小空间碎片探测器探头研究

MOS电容传感器具有结构简单、可靠、功耗小等优点,在国外已被成功用于微小空间碎片在轨探测,但国内开展的相关研究还较少。文章在对MOS电容传感器探测微小空间碎片原理及过程进行分析的基础上,基于ADS软件建立了传感器电路模型,确定了影响传感器探测性能的关键参数,完成了传感器的设计及研制,进而研制了阵列式探头。最后对阵列式探头成功开展了地面高速微粒撞击试验,探头在经过了数十次高速微粒撞击后,仍能对高速撞击事件进行测量,初步验证了使用该探头开展在轨微小空间碎片探测是可行的。     

基于无刷直流电机的电动车控制器研究与设计

传统的电动车用无刷直流电机(BLDCM)控制器功率逆变电路,为实时检测相电流,通过电阻进行相电流采样并反馈给微控制单元(MCU)进行电流环闭环控制,然而,在功率较大的控制器电路应用中,大电流会导致功率损耗增加。为解决这一问题,以STM32系列微型单片机为核心,设计了一套电动车控制器控制电路。重点阐述BLDCM硬件控制。为改进电源短路保护电路,提出了一种新型的MOS管内阻采样方法,并制作铝基板PCB。测试结果表明:该控制电路测控性能稳定,能够应用于工业生产中。     

模糊AHP法在机场最小起降带优选评价中的应用

机场最小起降带的选择 ,可视为多目标决策问题 ,采用层次分析法(AHP)求解。但实际研究过程中发现 ,最小起降带优选过程中所考虑的起降要求等因素多为带有模糊概念的标度 ,一般不易把握 ,而层次分析法中关于判断矩阵的一致性指标又常常难以达到。为解决上述问题 ,将模糊集合论与决策理论相结合的产物———模糊层次分析法 (FAHP)引入到了最小起降带优选模型中来 ,对影响因素的权值确定提出了新的方法。     

一种基于HVS的图像质量评价方法

通过充分分析人类视觉系统(HVS) 的亮度、纹理、边缘等特性, 给出相应的视觉特性计算模型,在此基础上提出一种结合HVS特性的加权峰值信噪比计算方法.实验结果表明该模型计算出的HVS值能充分反映人类视觉系统的屏蔽特性;图像质量评价方法的评价结果与主观评价结果相一致,效果优于传统图像质量评价方法.     

面向并行模拟机的path-CSA MOS开关模型及评价算法

提出一种新型MOS开关模型,它基于MOS CSA模型,又具有path MOS模型特性。新模型采用了逻辑门一级的Time-mapping事件驱动算法,有利于采用并行模拟机硬件实现。新算法利用了path MOS模型路径法特性,因而克服了CSA方法中的LOOP问题。新算法中首次提出最大、最小信号强度传送及评价操作,克服了MOS电路逻辑模拟中存在的不定值X问题。     

Optomechanical optimal design configuration and analysis of glue pad bonds in lens mounting for space application

Optomechanical systems are very complex requiring a high degree of accuracy. The carrier structure of an optical system is required to maintain the position of the optical components with respect to each other within the design tolerances. The most common loads on optical systems are self-weight, due to gravity orientations, and temperature ranges, due to exposure to rapidly changing temperatures from very cold to very hot and during launch. The fixing should ensure mechanical stability and thus accurate positioning in various gravity orientations.In order to ensure reliability during a space flight mission, the optomechanical engineer must understand the requirements of the space flight environment as well as the physics of failure of the optical components themselves; this can minimize the risks of on-orbit failure.This paper focuses on the optomechanical optimal design lens mounting using glue pads bonding. The main idea of this research study is to obtain an optimal choice of the position of the glue to fix the lenses on the barrel in such a way that we obtain a configuration of the optical assembly performance with less stress.In this paper, an investigation was performed using several methods including (thermo-elastic analysis, the margin of safety and lens distortion analysis). The results show that the position with six contacts glue pads is the best configuration compared to other configurations. This solution can be very helpful for decision-makers and optical engineers during the development phases of space optomechanical systems.