梯型螺母中径综合误差值分析

在机械传动中,梯形丝杠与大小螺母的配合是一种常见的结构,而梯形丝杠中的大、小螺母的加工又是一个关键问题,结合工程实际提出了梯型螺母在加工检验中存在的中径精度问题,并就此问题进行了详细讨论和理论分析,并且给出了解决问题的方法,对于同类零件的加工也具有指导意义.     

超声波流量计不同运算方式对比分析

温度漂移是影响超声波流量计测量精度的一个重要因素,本文从算法上提出一种不受其影响的数学模型,以使相应的硬件简单化.该方法已应用在超声波流量计中,收到了很好的效果.     

频率计数器在航天器信号频率测量中的适用性分析

从频率计数器的工作原理出发,分析了航天器测控通信中常用的调相信号、调频信号和相移键控信号的频率测量误差,给出了调相信号和调频信号的测量误差表达式。使用频率计数器对上述3种航天器信号进行了频率测量试验。理论分析和试验结果表明,频率计数器适用于航天器调相信号和调频信号的频率测量,不适用于相移键控信号的频率测量。在实际使用中,为保证测量精度,应根据被测信号的调制方式选择适当的测量方法。     

Minimum sliding mode error feedback control for fault tolerant small satellite attitude control

This paper proposes a new control strategy (which we call “minimum sliding mode error feedback control, MSMEFC”) for small satellite attitude control. As we know, the attitude control algorithm plays a significant role in the whole performance of the satellite, especially under the existence of uncertain disturbances from the space. Without loss of generality, the MSMEFC is presented based on the sliding mode theory. It is assumed that the equivalent control error is defined to offset the uncertain disturbances to improve the control performance. Hence, in order to estimate the optimal equivalent control error, a cost function is derived on the basis of the principle of minimum sliding mode error. Then, the equivalent control error wills feedback to the conventional sliding mode control to obtain the final MSMEFC. According to the theoretical analyzes, the sliding mode after the MSMEFC will approximate to the ideal sliding mode, resulting in enhancing the control performance. Moreover, an adaptive non-singular terminal sliding mode is employed to compare with the performance of MSMEFC. Several simulations are performed to verify the effectiveness of proposed MSMEFC in the presence of serious perturbations, even in some fault-tolerant scenarios.     

Cooperative guidance of seeker-less missile considering localization error

To perform an accurate fire-and-forget attack of seeker-less missile with the consideration of the localization error, a new cooperative guidance strategy of multi-missiles is proposed in this work. Firstly, an estimated position of the seeker-less missile is carefully selected, based on which the slant angle of the line between the estimated and real positions of the seeker-less missile is approximately derived inspired by the localization theory of GPS(Global Position System).Then, respectively based on the guidance law considering the impact angle and time constraints, the consensus theory and the finite-time convergence approach, three cooperative guidance laws employing the previously obtained slant angle are derived for intensive attack to address either a stationary or maneuvering target. Simulation results well demonstrate the effectiveness and advantages of the proposed cooperative guidance strategy.     

基于共轭次梯度算法的磁传感器安装误差校正

随着头盔显示技术的发展,对头盔电磁定位的精度要求越来越高,在现有的加工工艺和机上安装条件下,要提高定位精度,必须对传感器安装误差进行校正。通过坐标转换原理对安装误差进行建模,在此基础上利用最小二乘原则选取目标函数,将校正过程抽象为最优化问题求解。提出一种基于共轭次梯度算法的最优化问题求解方法,实现了传感器安装误差校正。利用MATLAB上对校正算法进行仿真,仿真结果表明,共轭次梯度算法简洁易用、校正精度高、收敛速度快,能够明显提高磁场测量精度。     

基于功率裕度的某型发动机全寿命性能研究

随着使用时间不断增加,研究飞行队所有选装ARRIEL2S系列发动机全寿命性能变化趋势的必要性突显.针对SRRIEL2S系列发动机全寿命性能参数变化特点,提出使用基于可几误差舍弃理论处理发动机功率校验数据,分区间描绘该系发动机全寿命性能指标变化趋势,给出该系发动机全寿命性能特点,为机务工程人员监控该系发动机提供有利依据；提出延长功率校验间隔的假设,并在理论上做了充分论证,为节约该系发动机运行成本提供一个明确及可行的方向.     

AHP中判断矩阵元素最优估计值的误差分析

在AHP模型中，请一组专家对某一属性进行评价，通过适当的数学处理方法，可得判断矩阵元素的最优估计值，并根据残差来确定所求估计值是否达到精度要求，若不符合精度要求则需返还给专家进行重新评估。这是AHP中构造判断矩阵的一种新方法。     

空心长轴深孔加工工艺研究

以某发动机空心长轴零件深孔加工为研究对象,设计了长径比为15,长度超过1米的整体硬质合金刀杆,在某加工项目试验中,应用这种超长整体硬质合金刀杆,在细长比大于10的空心长轴的深孔镗削加工中,改变了传统的深孔加工工艺,满足了空心长轴深孔加工中严格的壁厚差要求,取得了明显的效果.     

距离信息对DDFRC算法定位误差的影响与分析

在固定单站无源定位算法中,基于角度(Direct of Arrival)、角度变化率(Direct of Arrival Rate-of-Change)、多普勒频率(Doppler Frequency)和多普勒频率变化率(Doppler Frequency Rate-of-Change)4个观测信息实现定位(即DDFRC定位)算法仅通过单次观测即可实现对目标辐射源的定位。文中通过转移观测的卡尔曼滤波对定位结果进行平滑,较原有算法拥有更好的跟踪效果。同时,对定位误差进行了定量分析,并将距离信息引入算法的仿真分析之中,详细讨论了各个观测量误差在不同距离时对算法定位性能的影响,根据仿真结果,结合定位误差的定量分析对算法性能做出评价。通过仿真分析,得到了定位算法对不同距离下各参数的精度要求,从而为在实际系统中使用该定位算法提供了参考。