激光干涉信号的时域平均滤波处理

时域平均法是从混有噪声的信号中提取周期性分量的最有效方法.本文分析了时域平均法对光电信号进行滤波处理在激光绝对法校准振动传感器相频特性中的应用.通过对其原理的分析,证明了该方法在实现对有用信号滤波的同时也保证了信号的线性相位变化.     

利用Gaussian型RBF网络进行函数逼近的构造性估计

前馈人工神经网络有着极其广泛的应用，如何估计隐层神经元数及相应的逼近误差，一直是确定前馈网络结构的难点和关键。RBF网络是一种最重要的前馈网络，本文给出了利用Gaussian型RBF网络逼近连续函数或Lebesgue-可积函数时的构造性隐层单元数显式估算式及相应的显式逼近误差估算式。文中的结论也易于推广到离散样本的情形。这些结论对于提高Guassian型RBF在实际应用时的计算精度和减少计算量具有一定的指导意义。     

任意平面曲线的圆弧逼近方法

提出了一种根据给定精度逼近平面任意曲线的方法。该方法可以逼近任意次有理Ｂ样条曲线以及非均匀有理Ｂ样条曲线，尤其克服了双圆弧逼近方法的局限性实现了对封闭曲线的圆弧逼近。该方法独立于坐标系，独立于曲线类型。实际应用结果表明，它是一个适用于ＣＡＤ／ＣＡＭ集成系统任意平面曲线的圆弧逼近通用算法。本文对边界条件确定、误差修正和拐点处理进行了一定的研究，得出了一些价值性高、实用性强的结论，为数控加工任意平面曲线提供了一条简捷、易行、可靠的途径。     

16MnR钢疲劳统计特性评估的双随机变量方法

严格按照ASTM standard E647-93，对16MnR钢进行了21试件的紧凑拉伸试验，为了描述疲劳裂纹扩展统计特性规律，采用两个随机变量Paris公工描述疲劳裂纹扩展统计特性的方法，为了疲劳统计特性评估，采用了含双随机变量的Paris公式，二阶矩解法，与试验结果比较说明，所用方法的合理性。     

航天器拦截的输出协方差配置控制

本文通过对航天器拦截问题的分析，确定出系统输出在一定的方差约束下，系统反馈控制的设计目标。通过对［１］中提出的状态协方差控制理论的改造，给出了实现这一设计目标的方法，并提供了说明性的数值例子     

战术导弹级间线分离探讨

级间分离有点分离和线分离两类技术手段。线分离的优点很多,已日益广泛地应用于战略导弹中,并有逐步代替点分离的趋势。然而迄今为止,这种先进的技术还未应用于战术导弹中。文章分析了个中缘故,挑明了问题所在;提出了解决办法;例举了各种线分离装置的“饼式”结构图及其设计要领。     

离散时间线性系统的干扰不变性原理及其应用

本文在文献[1]的基础上讨论了具有直接或间接可测外干扰的离散时间线性系统的不变性问题。首先,在无约束的情形下,导得了系统输出保持完全不变性和终端不变性的条件,给出了干扰补偿系数的递推计算公式。然后,进一步讨论了外干扰向量和补偿向量幅值受约束时,系统保持不变性的条件。文中还给出了一个应用实例。     

Linear stability of ring systems around oblate central masses

In this paper, we consider the stability of a ring of bodies of equal mass uniformly distributed around a large oblate central mass. The purpose of this and previous papers is to shed light on the stability of Saturn’s rings. Previous papers have been limited by the assumptions that (1) all ring bodies are at the same distance from the central body, (2) the central body acts like a point mass (i.e., is a perfect sphere), and (3) the ring bodies all have the same mass and are evenly spaced around the ring. The third limitation is probably the least important; as long as there are a large number of masses and the mass distribution is approximately uniform then the system should behave as a system of equally-spaced, equal-mass bodies. The first main purpose of this paper is to remove the second limitation. But, the paper also aims to address limitation (1). Recent computer simulations of single-ring systems have shown that the threshold for stability, as determined by a linear stability analysis, matches precisely the stability threshold predicted by simulation. In other words, a linear stability analysis while presumably just a mathematical abstraction actually tells us something quite real. Furthermore, simulations of multi-ring systems suggest that instability comes from azimuthal perturbations; small azimuthal changes are more destabilizing that small radial perturbations. Hence, in this paper, we also consider the situation where the central body consists not just of an oblate central mass but also incorporates a flat ring representing in aggregate all ring bodies at radii other than the one under consideration. The central oblate body together with a flat ring is modeled simply by introducing two oblateness terms to the gravitational potential associated with the central mass. The subsequent analysis is almost identical to the case of a single oblateness term. For Saturn, the oblateness of the central mass is six orders of magnitude more significant than the rings at other radii as a destabilizing influence.     

Indirect Radau pseudospectral method for the receding horizon control problem

To solve the receding horizon control (RHC) problem in an online manner, a novel numerical method called the indirect Radau pseudospectral method (IRPM) is proposed in this paper. Based on calculus of variations and the first-order necessary optimality condition, the RHC problem for linear time-varying (LTV) system is transformed into the two-point boundary value problem (TPBVP). The Radau pseudospectral approximation is employed to discretize the TPBVP into well-posed linear algebraic equations. The resulting linear algebraic equations are solved via a matrix partitioning approach afterwards to obtain the optimal feedback control law. For the nonlinear system, the linearization method or the quasi linearization method is employed to approximate the RHC problem with successive linear approximations. Subsequently, each linear problem is solved via the similar method which is used to solve the RHC problem for LTV system. Simulation results of three examples show that the IRPM is of high accuracy and of high compu-tation efficiency to solve the RHC problem and the stability of closed-loop systems is guaranteed.     

轻型飞机燃油油量表指示器的原理设计和定量分析

燃油油量的测量，方法很多。本文首先论述了浮子电位器式传感器与电阻电桥相匹配的测量原理以及计算方法，