超声波马达技术及其应用

对超声波马达技术及其应用现状和发展前景做了介绍。     

二元混压超声速进气道三维流动数值分析

按照MacCormack时间分裂方法，应用NND格式、对流迎风矢通量分裂（AUSM）技术和Baldwin-Lomax混合长度代数湍流模型，对贴体坐标下三维雷诺平均N－S方程进行有限差分离散。数值计算了均匀来流和非均匀来流条件下二元混压超声速进气道三维湍流流动态，分析了该进气道主要性能参数随出口反压、来流马赫数、导弹工作高度及飞行攻角的变化特性，为深入研究进气道性能提供了一定辅助手段。     

Estimating the Doppler centroid of SAR data

After reviewing frequency-domain techniques for estimating the Doppler centroid of synthetic-aperture radar (SAR) data, the author describes a time-domain method and highlights its advantages. In particular, a nonlinear time-domain algorithm called the sign-Doppler estimator (SDE) is shown to have attractive properties. An evaluation based on an existing SEASAT processor is reported. The time-domain algorithms are shown to be extremely efficient with respect to requirements on calculations and memory, and hence they are well suited to real-time systems where the Doppler estimation is based on raw SAR data. For offline processors where the Doppler estimation is performed on processed data, which removes the problem of partial coverage of bright targets, the ΔE estimator and the CDE (correlation Doppler estimator) algorithm give similar performance. However, for nonhomogeneous scenes it is found that the nonlinear SDE algorithm, which estimates the Doppler-shift on the basis of data signs alone, gives superior performance     

功率MOSFET逆变器在VSCF电源中的应用

 以用于交直交飞机VSCF电源系统的SPWM逆变器作为研究对象。利用数字计算机对自然采样SPWM过程进行了数值分析,得到SPWM逆变器输出电压频谱与脉宽调制参数(M、N)之间的关系。同时,数值分析考虑了GTR存贮时间t_s和导通延迟时间t_0对SRWM频谱的影响。选择新型功率开关器件—功率MOSFET构成小容量VSCF电源的逆变器。并给出两种高效、可靠的功率MQSFET栅极驱动电路及逆变器的试验特性,     

I-O map inversion, zero dynamics and flight control

The trajectory control of aircraft in rapid, nonlinear maneuvers is discussed. Based on nonlinear invertibility theory, a control law is derived to independently control roll, pitch, and sideslip angles using rudder, elevator, and aileron. Integral feedback is introduced in order to obtain robustness in the control system to parameter uncertainty. The stability of the zero dynamics is examined. Simulation results are presented to show that in a closed-loop system, precise simultaneous lateral and longitudinal maneuvers can be performed despite the presence of uncertainty in the stability derivatives     

Huygens' Surface Science Package

The design and performance of the Surface Science Package (SSP) on the Huygens probe are discussed. This instrument consists of nine separate sensors that are designed to measure a wide range of physical properties of Titan's lower atmosphere, surface, and sub-surface. By measuring a number of physical properties of the surface it is expected that the SSP will be able to constrain the inferred composition and structure of the moon's near-surface environment. Although the SSP is primarily designed to sense properties of the surface, some of its sensors will also make measurements of the atmosphere along the probe's entry path and will complement the data gathered by other experiments on the Huygens probe. This revised version was published online in August 2006 with corrections to the Cover Date.     

Analysis of generalized guidance laws for homing missiles

It is shown that the optimal guidance problem can be handled as a Bolza-type problem which can be solved by straightforward calculation. The solution proves to be different from that given by Yang, et al. (1989) and is verified to be a minimum performance index solution. Also presented is an alternate unified approach to the solution of the nonlinear system of differential equation of the generalized proportional navigation law discussed earlier by Yang, et al. This unified equation has been solved for all the different cases of proportional navigation for which closed-form solutions have been published by earlier authors     

绕凸台的高超声速分离流动研究

本文研究高超声速流动绕三维低凸台的流动特性。凸台高度与边界层厚度之比介于0.5～0.8,凸台周边倾角介于14°～45°。在高超声速风洞中,来流马赫数为5,单位雷诺数为2.6～6.0×10~7/米。实验过程中测量了模型中心线及特殊部位之表面压强分布,根据纹影记录及表面流动显示确定激波与边界层干扰流场特性及分离区的变化。发现分离区在中心线上距凸台最远,而在凸台肩部距周边沿法线方向最近,确定了中心线上最大压强比的位置。     

Sensor Fault Detection in a System with Random Disturbances

Sensor faults are detected in an operating automatic system by a simplified version of the dedicated observer scheme. Control inputs are augmented by a random disturbance of moderate intensity. The dedicated observer in this case is a Kalman filter, driven by a single sensor. This filter provides estimates of the outputs from the other, nonredundant, sensors. A logical combination of these functionally redundant signals with the actual sensor signals provides prompt detection of incipient faults on all instruments without false alarms. The scheme is applied to a simulation of the lateral axis control system of a hydrofoil boat in which four sensors are to be covered by the fault detection scheme. Tests indicate that the scheme is robust with respect to variations in the intensity of the random disturbance.     

网格分区构筑中区域边界的隐式处理方法

介绍一种网格分区构筑中区域边界的隐式处理方法──ADMZI法。该方法具有简单实用、数据结构灵活等特点,特别适合于区域边界难以确定的情况。将该方法应用于多级火箭级间分离时的流场物理域网格构筑,结果证明是成功的。