An approach for parameter estimation of combined CPPM and LFM radar signal

In this paper, the problem of parameter estimation of the combined radar signal adopting chaotic pulse position modulation (CPPM) and linear frequency modulation (LFM), which can be widely used in electronic countermeasures, is addressed. An approach is proposed to estimate the initial frequency and chirp rate of the combined signal by exploiting the second-order cyclostationarity of the intra-pulse signal. In addition, under the condition of the equal pulse width, the pulse repetition interval (PRI) of the combined signal is predicted using the low-order Volterra adaptive filter. Simulations demonstrate that the proposed cyclic autocorrelation Hough transform (CHT) algorithm is theoretically tolerant to additive white Gaussian noise. When the value of signal noise to ratio (SNR) is less than 4 dB, it can still estimate the intra-pulse parameters well. When SNR = 3 dB, a good prediction of the PRI sequence can be achieved by the Volterra adaptive filter algorithm, even only 100 training samples.     

SINS基于非线性量测的大失准角初始对准算法

针对陆用捷联惯导系统(SINS)大失准角初始对准问题,提出一种基于二阶非线性量测的二阶泰勒级数展开的初始对准算法。首先,将大失准角非线性对准问题,转化为具有线性系统方程和二阶非线性量测方程的滤波问题。然后,设计基于二阶非线性量测方程的二阶泰勒级数展开的滤波算法,可以在任意姿态和无初值条件下进行初始对准和参数估计。最后进行车载对准试验,结果表明,新算法可以在300s内完成实现大失准角初始对准,对准精度与传统分段对准算法相当。     

确定时间序列均值和方差函数的移动多点平均方法

为了提高有限样本或小样本情况下时间序列均值和方差函数的确定精度,以保证时序建模、分析和预测精度,提出一种确定序列趋势项的移动多点平均方法.该方法能够得到时间序列均值中非周期部分,结合样本周期图法得到的周期项,可综合得到其均值函数,并可进一步得到时序的标准差函数.Monte Carlo模拟对比结果表明:该方法不仅能够保证时间序列段内分析精度,而且能够有效提高时间序列的预报精度.      

一种非规则采样航空时序数据异常检测方法

航天器遥测数据的实时异常检测对于航天任务具有重要意义。以往方法大都考虑规则采样且缺失率较低的时序数据,然而航空时序数据具有维度大、噪声多、缺失率高、采样间隔不规则等特点,因此异常检测任务较为困难。针对非规则采样且具有缺失值的多维航空时序数据提出非规则采样多维时序数据异常检测（IMAD）算法。首先,采用带有可训练迟滞项的门控循环单元（GRU-D）对缺失值和非规则采样的时序数据进行建模;然后,采用变分自编码器建立随机性模型,学习正常时序数据的分布,从而对噪声数据具有鲁棒性;最后,利用基于极值理论的自适应阈值确定法确定合适阈值进行异常检测。结果显示,在两个真实航空时序数据集上,IMAD具有超出当前最新异常检测算法的性能;多个实验表明,IMAD在缺失率、参数以及数据集变化时,能够维持较好的异常检测效果,具有较强的鲁棒性。     

Monitoring of the space system

We have performed monitoring of the space system that includes the Earth, the Moon, the Sun, and the GPS satellite group. We have discovered semi-diurnal and diurnal periodicities in the number of satellites detected as well as in the altitude, latitude and longitude by a GPS receiver. We have revealed tidal deformations related to changes in the Earth?s orientation with respect to the Moon and the Sun.     

DPOD2014: A new DORIS extension of ITRF2014 for precise orbit determination

To support precise orbit determination of the altimetry missions, the International DORIS Service (IDS) regularly estimates the DPOD (DORIS terrestrial reference frame for Precise Orbit Determination) solution which includes mean positions and velocities of all the DORIS stations. This solution is aligned to the current realization of the International Terrestrial Reference Frame (ITRF) and so, can be seen as a DORIS extension of the ITRF. In 2016, moving to the IDS Combination Center, the DPOD construction scheme changed. The new DPOD solution is produced from a DORIS cumulative position and velocity solution. We present the new methodology used to compute DPOD2014 and its validation procedure. In order to present geophysical applications and interpretations of these results, we show two examples: (1) the Gorkha earthquake (M7.8 – April 2015) generates a 3-D mis-positioning of nearly 55?mm of the EVEB DORIS station at the Everest base camp 90?km from the epicenter. (2) Applying the results the DPOD2014 realization, we show that the most recent vertical velocity of Thule, Greenland is similar to that observed between 2006 and 2010, indicating further ongoing ice mass loss in the Thule region of northwest Greenland.     

无源器件无源互调干扰行为建模

无源互调干扰会影响多载波通信卫星的正常工作,是目前卫星通信系统必须考虑的问题之一。由于无源互调干扰问题具有一定的复杂性,无法直接分析无源互调分量,因此需要建立相应的模型进行研究。针对无源互调干扰的频率分布特点,采用双指数函数模型和Volterrra级数模型拟合无源互调干扰,推导并建立了QPSK调制信号的无源互调干扰时序模型。基于MATLAB的仿真结果表明,无源互调干扰分量的理论值频点处都出现了相应峰值,且其幅度值与输入信号中心频率处的幅度值的比例符合理论分析。     

带多充液圆柱贮箱航天器刚-液耦合动力学研究

文中以在低重环境下带多充液圆柱贮箱刚性航天器中刚-液耦合方程的建立和求解为主要研究目的。推导航天器中充液圆柱贮箱内任意点的牵连运动方程,根据壁面边界条件给出了贮箱内液体牵连晃动势的表达式;利用第二类边界条件下的傅立叶-贝塞尔级数展开法对低重力环境下的弯曲自由液面处的复杂动力学边界条件进行处理,建立以液体相对晃动势的模态坐标和晃动波高的模态坐标为状态向量的液体耦合晃动力学方程,通过积分分别得到了耦合晃动力和耦合晃动力矩的解析式;运用准坐标系下的拉格朗日方程建立以航天器主刚体姿态坐标和轨道坐标为状态向量的刚体耦合运动动力学方程,进一步联立上述耦合方程得到航天器整体系统的刚-液耦合动力学状态方程;最后,编制出适用于带多充液圆柱贮箱航天器内刚-液耦合动力学计算的模块化计算程序,通过计算实例验证所编程序的准确性的同时,研究了携带多充液箱航天器系统贮箱布局、外激励方式对航天器刚-液耦合系统动力学特性的影响。     

Optimal solar sail trajectory approximation with finite Fourier series

The heliocentric transfer of a solar sail-based spacecraft is usually studied from an optimal perspective, by looking for the control law that minimizes the total flight time. The optimal control problem can be solved either with an indirect approach, whose solution is difficult to obtain due to its sensitivity to an initial guess of the costates, or with a direct method, which requires a good estimate of a feasible (guess) trajectory. This work presents a procedure to generate an approximate optimal trajectory through a finite Fourier series. The minimum time problem is solved using a nonlinear programming solver, in which the optimization parameters are the coefficients of the Fourier series and the positions of the spacecraft along the initial and target orbits. Suitable constraints are enforced on the direction and magnitude of the sail propulsive acceleration vector in order to obtain feasible solutions. A comparison with the numerical results from an indirect approach shows that the proposed method provides a good approximation of the optimal trajectory with a small computational effort.     

动态系统元器件失效率的矩独立重要性测度分析

针对不确定性元器件失效率对动态系统失效概率影响程度的度量问题,研究了动态系统元器件失效率的重要性分析方法。分析了不确定性情况下动态系统失效概率的特点;依据Borgonovo的矩独立灵敏度分析思想,提出了两种新的矩独立不确定性重要性测度,给出了基于蒙特卡罗数值仿真的一般求解方法,分别用来分析系统工作时间给定和在区间变化两种情况下元器件失效率不确定对系统失效概率分布函数的贡献程度;建立了重要性测度的高效算法,通过稀疏网格积分技术将多元函数的积分问题转化成一元函数积分的张量积组合,通过Edgeworth级数方法将响应量分布函数的求解问题转化为基于其前四阶矩的失效概率估计,从而有效降低了功能函数的调用次数,提高了重要性测度的求解效率。最后,通过两个算例验证了所提方法的合理性和算法的高效性。