Modified Barker and Huffman Sequences in Combination Codes

lt is possible that usable combination codes can be obtained if Barker and Huffman sequences are chosen as the inner and outer codes. lt is shown that an improvement in either energy efficiency or time sidelobe structure will result either from a modification of a Huffman sequence or from a modification of a Barker sequence. Results are given for a combination code of length 91, with inner and outer codes of length 7 and 13.     

任意K元Huffman树的新构造

给出了一种简单而有效地构造任意k元最优Huffman树的新方法。给出了Huffman村存贮的父母一子女环结构,该结构空间利用率高,在不增加parent域的情况下,使查找父母的T（m）达到O（1）,并能高效实现建立最优Huffman树和求Huffman编码的算法,无论是空间复杂度还是时间复杂度均优于传统算法,具有很强的实用性。     

The Design of Huffman Sequences

The paper presents a method by which the zeros of the polynomial representing a Huffman (impulse-equivalent) pulse sequence can be chosen so as to exert a degree of control on the form of the energy distribution of the signal in the time-frequency plane. This makes it possible to design Huffman pulse sequences which are suitable for use as radar or sonar signals in situations where significant target velocity occurs.     

数列算术平均序列的收敛性

对一般数列的情况进行了讨论,给出了数列的子列权的概念,得出了关于数列的算术平均序列的一个定理,即存在有限划分的收敛子列的数列,其算数平均序列收敛于其子列极限的线性组合,而系数正是相应子列的权。对其他的一些情况也进行了讨论。     

基于小波变换的混和压缩编码

根据数字图像编码的现状，在分析目前图像压缩的常用方法优缺点的基础上，采用小波变换，对不同视觉敏感的频段采用不同分辨率的量化同时，结合非均匀量化和Huffman编码，对图像进行混合编码压缩，获得了好的压缩效果。     

Automatic target recognition using sequences of high resolutionradar range-profiles

In this paper, we address the problem of joint tracking and recognition of a target using a sequence of high resolution radar (HRR) range-profiles. The likelihood function for the scene configuration combines a dynamics-based prior on the sequence of target orientations with a likelihood for range-profiles given the target orientation. A deterministic model and a conditionally Gaussian model for range-profiles are introduced, and the likelihood functions under each model are compared. Simulations are presented demonstrating recognition of mobile aircraft and ground targets, and results showing performance of the algorithm are given in terms of the expected angular estimation error and the rate of correct recognition     

函数列一致收敛的一个判定方法及其性质

给出了一个定理用于判定函数列的一致收敛,通过此判定定理,又得出了由一致收敛函数列构造新的一致收敛函数列的几个性质。     

结构的最优预防性维修周期

提出了一种计算结构最优预防性维修周期的模型。首先将结构的初始损伤、使用过程中的损伤累积用主裂纹长度的分布加以定量描述。针对预防维修只能在离散的时间点上进行的结构,考虑结构的失效损失费和维修费用,根据使结构单位使用时间的费用（费用率）达到最小的原则,建立了选择最优预防维修周期的方法。最后对一结构作了具体计算。     

Presupernova evolution of the most massive stars

Taking as example a 60M _⊙ star of solar metallicity, the state of the art of model calculations for very massive, from the main sequence to the supernova stage, is reviewed. It is argued that — due to the simple internal structure of Wolf-Rayet stars — the post main sequence evolutionary phases are currently those which are better understood. A brief discussion of the supernova outcome from very massive stars is given. Then, the more uncertain main sequence evolution is discussed. A first attempt to incorporate results about pulsational instabilities of very massive stars in stellar evolutionary calculations is performed. On its basis, a new type of evolutionary sequence for very massive stars is obtained, namely O-star → Of-star → H-rich WNL → LBV → H-poor WNL → WNE → WC → SN. This scenario is shown to correspond better to many observed properties of very massive stars than the standard one. It includes a model for the prototype LBV P Cygni.     

Bias and Standard Deviation of the Estimator for the Underlying Probability in a Sequence of Bernoulli Trials with Preselected Number of Successes

In a sequence of Bernoulli trials which stops after a preselected number M of successes, the maximum likelihood estimator of the underlying probability is given by the ratio of M and the required number of observations. Closed-form expressions for the bias and standard deviation of this estimator are developed.     

基于进离场流量和冲突发生位置的扇区规划

随着空中交通流量的日渐增大，空域结构及交通流分布的不合理性导致空中交通管制与飞行安全存在着一定的隐患。鉴于机场进近区是限制空域运行能力的主要瓶颈，针对如何提高空域资源利用率从而提升空域容量进行了进近区扇区规划，提出了考虑飞行流量、冲突发生的位置以及空域运行情况等因素建立的扇区容量均衡模型，利用霍夫曼编码原理进一步找到了扇区边界，并验证了方法的科学性和合理性。     

绕非对称头锥的分离系数矩阵差分法

一、亚跨区SCM方法 （一）基本方程和边界条件 建立在球坐标下无因次化的拟非定常欧拉方程组为     

Quasi-Complementary Sequences

A method of constructing digital phase reversal codes which have few nonzero sidelobes and which are available in frequent lengths is given. This is particularly important in the area of longer codes. The codes are a form of combined sequence and, hence, have the desirable property of bandwidth reduction for the outer code. However, only two member codes are required. A major usage of these codes may be in addressing.     

切换线性奇异系统能达的必要条件

在各子系统正则的条件下研究了切换线性奇异系统的能达性问题。对给定的切换序列定义了容许控制集合,以保证在该容许控制集合中的任意控制律的作用下,相应切换系统的状态都是连续的。基于切换线性奇异系统状态方程解的结构特点,定义了一系列子空间。利用所定义的子空间是循环不变子空间的特点,得到了切换线性奇异系统能达的必要条件。所给的必要条件涵盖了常规切换系统和非切换奇异系统的能达性必要条件。     

基于遗传算法的飞机维修拆卸/装配序列规划研究

飞机维修拆卸/装配序列规划是整个飞机产品维修作业的重要组成部分,同时也是飞机远程诊断与远程维修的重要研究内容。针对飞机维修过程中拆卸/装配序列规划问题的特点和要求,本文从维修产品的拆卸/装配过程稳定性、拆卸/装配方向和拆卸/装配工具的改变次数三个方面来设置目标函数,解决了零件数量大的产品规划计算效率不高且没有考虑产品的维修过程稳定性问题。本文开发出了基于遗传算法的飞机维修拆卸/装配序列规划系统,并结合具体产品进行了验证。     

飞机电子防滑刹车系统模拟仿真

提出用飞机三自由度模型进行防滑系统的仿真研究,给出某型飞机的刹车曲线。     

Modeling Nonstationary Random Processes with an Application to Gyro Drift Rate

The problem of estimating the a priori statistics of a nonstationary process is considered using finite-time averages of experimental data. A model of the form of a linear time-invariant difference equation with a stationary independent random sequence driving function is proposed and investigated. Finite-time averages are calculated and then used in a steepest descent method to determine the coefficients of the difference nce equation. Methods are presented for transforming this model to the statespace pace format necessary for Kalman filtering, and an example is given using actual gyro drift-rate data.     

10 Gbit/s伪随机序列光纤通信系统PMD补偿

光纤通信线路检测到的电功率随差分群延迟变化,可作为PMD补偿的反馈控制信号。给出了这一变化关系的理论计算和曲线并通过实验验证这一关系,确定电压信号与DGD的变化关系。建立了一套完整的实验系统,并考虑了影响反馈电压信号的多种因素以及减小这些影响的措施。通过眼图给出的实验结果说明了补偿的效果,还通过误码测试仪测量了补偿前后的接收灵敏度的改变以定量说明补偿的效果,最后比较了不同情况下的补偿结果。     

终端区域4D导引的高度剖面与速度剖面研究

对终端区域４Ｄ导航中高度剖面和速度剖面生成的基本算法进行了研究。结合已经开发的水平轨迹计算方法,生成终端区域的３Ｄ飞行剖面和速度剖面,然后产生４Ｄ导航指令,利用已生成的４Ｄ导航指令可在终端区域引导沿直线或曲线飞行的飞机在规定的时间到达指定地点,从而实现终端区域的４Ｄ导引。最后对某民航运输飞机进行了数值模拟,由计算中看出风对４Ｄ导航的速度剖面有较大的影响,结果还表明该方法计算量小,只需输入少量的参数     

Electrooptical navigation for aircraft

Concurrently with the development of guidance laws for low-altitude rotorcraft flight operations, efforts are underway to develop automated systems for locating the terrain and the obstacles using inputs from passive electrooptical sensors such as TV cameras and infrared imagers. A passive obstacle location algorithm that uses image sequences from cameras undergoing translational and rotational motion is developed. The algorithm is in a general form and can operate in multicamera imaging environments. Performance results using an image sequence from an airborne camera are given