Research on nonlinear model predictive control for turboshaft engines based on double engines torques matching

In order to reach a compromise between fast response control and torques matching control in double turboshaft engines, research on nonlinear model predictive control for turboshaft engines based on double engines torques matching is conducted. Meanwhile, a Nonlinear Model Predictive Control (NMPC) method is proposed, which combines the control index of the power turbine speed with torques matching of double engines creatively. In addition to the control index, the difference of output torques between each engine is also incorporated in the objective function as a penalty term to ensure constant speed control and short torques matching time. Simulation results demonstrate that relative to unilateral torques matching, the settling time of the bidirectional matching method can be reduced by nearly 30.8%. Nevertheless, compared with the bidirectional torques matching method under the cascade PID controller, the NMPC method can decrease the overshoot of the power turbine speed by 65% and reduce the matching time by 15.5% synchronously. Besides fast response control of turboshaft engines, fast torques matching control of double engines is accomplished as well.     

激光等离子体天线的电磁散射分析

根据激光等离子体天线工作原理给出了电磁分析模型,以电场作为未知函数建立了频域体积分-微分方程,用脉冲基函数和点匹配函数的矩量法（MOM）将之转为线性代数方程组。求解中应用快速傅里叶变换（FFT）和共轭梯度法（CGM）,以降低所需计算机内存和减少CPU计算时间。算例表明：该法计算的结果与Mie级数解析解和其他文献结果吻合较好。     

A new approach to solar wind monitoring

The monitoring of solar wind parameters is a key problem of the space weather program. We are presenting a new solution of plasma parameter determination suitable for small and fast solar wind monitors. The first version will be launched during the SPECTR-R project into a highly elongated orbit with apogee ∼350,000 km. The method is based on simultaneous measurements of the total ion flux and ion integral energy spectrum by six identical Faraday cups. Three of them are dedicated to determination of the ion flow direction, the other three (equipped with control grids supplied by a retarding potential) are used for determination of the density, temperature, and speed of the plasma flow. The version under development is primarily designed for the measurements in the solar wind and tail magnetosheath, thus for velocities range from 270 to 750 km/s, temperatures from 1 to 30 eV, and densities up to 200 cm⁻³. However, the instrument design can be simply modified for measurements in other regions with a substantial portion of low-energy plasma as a subsolar magnetosheath, cusp or low-latitude boundary layer. Testing of the engineering model shows that the proposed method can provide reliable plasma parameters with a high time resolution (up to 8 Hz). The paper presents not only the method and its technical realization but it documents all advantages and peculiarities of the suggested approach.     

快速富里叶变换在计算柔性喷管频率特性中的应用

介绍了利用快速富里叶变换(FFT)计算离散数学模型频率特性的方法。经实例证明,此法误差小,计算效率高,完全能够满足工程上的需要。     

基于空间距离的快速稳健子空间跟踪方法

从空间距离的角度分析子空间跟踪问题,提出了一种新的子空间跟踪算法。提出的算法同时适用于信号和噪声子空间跟踪,而复杂度仅为3NL+O(N)。仿真表明算法对基的正交偏离稳健,对舍入误差不敏感,是一种快速稳健的子空间跟踪算法。     

基于快速终端滑模的航天器自适应容错控制

针对存在不确定的执行机构部分失效故障和未知外界扰动的航天器姿态跟踪控制问题,提出了一种基于自适应快速终端滑模控制的容错控制方法。在没有故障检测与诊断信息的情况下,采用快速终端滑模控制原理,利用自适应算法在线估计得到的故障信息,设计具有鲁棒性的容错控制器,使系统在执行机构故障发生时,能在有限时间内以指数收敛,实现系统有限时间渐近稳定,以及对航天器的容错控制和干扰的抑制。仿真结果表明,与基于普通滑模控制器的容错控制相比,该方法在保证系统鲁棒性和可靠性的同时,具有更快的收敛速率,实现执行机构故障时有效的航天器姿态跟踪控制。     

基于IRAPF算法的航天器姿态确定

针对航天器姿态确定系统中存在较大初始误差及非线性较强的问题,提出了一种基于改进的正则化辅助粒子滤波（IRAPF）算法的航天器姿态确定方法。该算法将正则粒子滤波（RPF）与辅助粒子滤波（APF）相结合,将快速高斯变换（FGT）方法引入其中以减少计算量提高滤波的收敛速度。算法不仅有效地抑制了粒子退化问题,而且利用最新观测粒子来优化采样,并且在引入FGT后计算量与正则化的辅助粒子滤波相比降低了30%,改善了滤波的实时性。仿真结果表明了滤波的有效性。     

一种中高速突发QPSK数字解调系统捕获与载波同步算法的研究

文章介绍了一种中高速突发解调处理系统突发捕获与载波同步算法实现,采用相位域突发捕获与同步算法,解决了卫星上行信号幅度变化对突发捕获解调性能的影响,具有突发捕获概率高、载波同步快和解调动态范围大等优点,并且该算法FPGA逻辑资源占用及运行速度在软硬件实现上具有很大优势。     

跨声速涡轮轮缘复合封严结构的数值研究

为了保护航空发动机涡轮盘,阻止高温燃气向盘腔内部深入,破坏核心部件,通常将压气机冷气引入转静盘腔,以抵抗高温燃气入侵,并对涡轮部件进行冷却。本文利用非稳态与稳态数值计算方法,研究了跨声速涡轮设计工况(Reφ＞107)下的两种复合封严结构：静盘存在封严环的覆叠封严和动盘带封严齿的咬合封严结构,并与轴向封严结构进行对比。在本文所研究的范围内,对非稳态计算进行快速傅里叶变换(FFT)的结果表明：跨声速涡轮流动中,叶栅通道存在由激波引起的高压区,导致了燃气的剧烈入侵,因此在特征信号频谱中f/fblade=2处存在峰值,这是跨声速涡轮燃气入侵最显著的特点。稳态计算证明复合封严结构封严性能良好。静盘封严环将盘腔分割为上下两个容腔,入侵容腔滞留了绝大部高温燃气,因此高半径处封严效率较低,但盘腔低半径处封严效率明显提高,在Cw≈996时,两种复合封严结构在r/b=0.96以下都能达到很高的封严效率。咬合封严能够增加燃气流动阻力,有效减小封严冷气使用量。但是两种封严结构在当冷气流量系数从Cw=199逐渐增大到2000时,高半径处封严效率并没有明显的提高,封严效率仅提高了20%~30%。     

高动态下基于DMF的伪码捕获频差估计研究

基于数字匹配滤波器（DMF）的PN码捕获电路具有较快的捕获速度,但其输出主相关峰值对频差较为敏感。为了消除频差对捕获性能的影响,文章提出了一种基于FFT的频差估计算法。首先构造一个载波频差的希尔波特复矢量,然后对其进行快速傅里叶变换。该算法能够精确检测出载波频偏的绝对值大小和方向,可以有效地改善大频差下的伪码捕获性能。