纤维缠绕结构的一种可靠性优化设计方法研究

将纽曼级数展开的蒙特卡罗随机有限元应用于具有随机因素的纤维缠绕结构的应力求解;然后利用蒙特卡罗直接比较法和蔡希布（Ｔｓａｉ－Ｈｉｌｌ）失效判据给出该结构的可靠性算式,最后建立了此类结构的可靠性优化设计迭代法,并给出了一算例。     

GPS时间比对数据的Vondrak平滑和三次样条插值处理

介绍了Vondrak平滑方法和三次样条插值方法。利用国家授时中心时间频率基准重点实验室的GPS时间比对数据,先进行预处理和规范化处理,再采用Vondrak平滑方法和三次样条插值方法进行处理,得到的结果表明:在实际中利用Vondrak平滑方法和三次样条插值方法对GPS时间比对数据处理是可行的,减弱了随机噪声的影响。     

基于支持向量机的航空发动机滑油监控分析

提出了一种基于支持向量机的航空发动机滑油金属含量预测方法。详细分析了支持向量机用于时间序列预测的理论基础,并给出了运用支持向量回归进行多步预测的一般公式,提出了用最终预报误差(FPE)准则优化选取嵌入维数。与传统的AR预测模型相比,支持向量机由于采用了新型的结构风险最小化准则表现出优秀的推广能力。经过数值仿真得出自回归(AR)模型仅适合于短期预测;支持向量机预测推广能力强、具有较强的鲁棒性和容错性,对较长区间预测仍具有较好的效果。最后,将其应用于某型发动机滑油的铁金属含量预测,取得了较好的效果。      

一种基于时间梳技术的高频正弦信号相位差测量方法

本文研究了一种基于时间梳原理的高频正弦信号相位差测量方法,给出了时间梳原理的数学模型,并详细分析了其特点,并将此原理首次应用于高频信号的数据采集中,可以用低频和被测信号构建一种高频等效采样技术,可以在不满足乃奎斯特采样定理下,对被测两路正弦信号进行同步采样,避免了高频信号采样的高采样率,结合多重互相关技术,实现了对高频正弦信号的相位差的高精度测量,实验结果表明本文算法对高频信号对高频正弦信号的相位差测量具有很高的测量精度,尤其在低信噪比下也有较高的测量精度,具有较高的工程实用价值。     

CHAMP卫星加速度计标校参数序列的谱分析

给出了利用能量守恒方法求定CHAMP卫星加速度计标校参数的基本原理和算法．对2001年8月-2003年12月共约两年半的CHAMP卫星加速度计数据进行了标校,导出了尺度、偏差和偏差漂移参数的时间序列,分别采用最小二乘谱分析和抗差谱分析对这些时间序列进行了分析．结果表明,尺度、偏差和偏差漂移参数都有明显的周期变化,但各主周期项略有差异．尺度的主周期是441d、220d、126d和13．4d的周期变化,其中220d和441d的周期变化的贡献相对较大．偏差中有明显的220d、126d和13．4d周期变化,各周期变化的贡献几乎相当;偏差漂移的主周期是220d、13．4d和9d的周期变化,其中13．4d的周期变化最为显著,几乎比其他周期项变化高出一个数量级．另外尺度和偏差参数还有明显的长期变化,而偏差漂移参数的长期变化不明显．     

地月空间星地双向单程测量高精度模型

针对使用星地双向单程测量技术实现给定场景下的地月空间高精度测量问题,建立了地月空间纳秒级星地时差解算模型与米级瞬时距离解算模型,定量分析了模型中各因素的量级,并对模型中收发时延、引力时延、定轨误差和大气延迟等多种因素引入的时差和距离估算误差进行了定量分析。仿真数据的处理结果校验了误差量级理论分析的准确性,时差估算的均方根误差优于7.6ns,瞬时距离估算均方根误差优于2.4 m。建立的模型可以对地月空间星地DOWR测量数据进行高精度处理,实现地月空间高精度时间比对,支持未来中国载人登月等任务及地月空间高精度导航技术。     

Shaping low-thrust trajectories with thrust-handling feature

Shape-based methods are becoming popular in low-thrust trajectory optimization due to their fast computation speeds. In existing shape-based methods constraints are treated at the acceleration level but not at the thrust level. These two constraint types are not equivalent since spacecraft mass decreases over time as fuel is expended. This paper develops a shape-based method based on a Fourier series approximation that is capable of representing trajectories defined in spherical coordinates and that enforces thrust constraints. An objective function can be incorporated to minimize overall mission cost, i.e., achieve minimum $\mathrm{\Delta }V$. A representative mission from Earth to Mars is studied. The proposed Fourier series technique is demonstrated capable of generating feasible and near-optimal trajectories. These attributes can facilitate future low-thrust mission designs where different trajectory alternatives must be rapidly constructed and evaluated.     

Time delay compensation in lateral-directional flight control systems at high angles of attack

The previous studies of time delay compensation in flight control systems are all based on the conventional aerodynamic derivative model and conducted in longitudinal motions at low angles of attack. In this investigation, the effects of time delay on the lateral-directional stability augmentation system in high-α regime are discussed based on the $\dot{\beta }$ model, which is proposed in our previous work and proved as a more accurate aerodynamic model to reveal the lateral-directional unsteady aerodynamic characteristics at high angles of attack. Both the $\dot{\beta }$ model and the quasi-steady model are used for simulating the effects of time delay on the flying qualities in high-α maneuvers. The comparison between the simulation results shows that the flying qualities are much more sensitive to the mismatch of feedback gains than the state errors caused by time delay. Then a typical adaptive controller based on the conventional dynamic derivative model and a gain-prediction compensator based on $\dot{\beta }$ model are designed to address the time delay in different maneuvers. The simulation results show that the gain-prediction compensator is much simpler and more efficient at high angles of attack. Finally, the gain-prediction compensator is combined with a linearized $\dot{\beta }$ model reference adaptive controller to compensate the adverse effects of very large time delay, which exhibits excellent performance when addressing the extreme conditions at high angles of attack.     

基于经验模分解的PPP时间比对数据消噪方法

精密单点定位(PPP)时间比对数据会受到观测噪声的影响,因此对时间比对数据进行消噪是一项重要工作。提出一种基于经验模分解(EMD)的PPP时间比对数据消噪方法,并将该方法与Vondrak滤波方法的消噪效果进行对比。结果表明,两种方法的消噪效果相当,均能有效滤除PPP时间比对数据中的随机噪声,明显改善时间比对的稳定度。