基于ECEF的误差配准与目标跟踪算法

考虑量测噪声和地球曲率对配准的影响,提出了一种基于地心坐标系(ECEF)的扩展卡尔曼滤波(EKF)配准与目标艰踪算法.根据坐标系转换关系,给出误差配准计算公式,建立目标的动态方程,用EKF方程进行估计.仿真结果表明:该法能同时有效估计目标运动状态和传感器配准误差,可用于远距离的传感器配准和目标跟踪.     

Simultaneous spacecraft attitude and orbit estimation using magnetic field vector measurements

Based on magnetometer measurements only, three-axis attitude, rate, and orbit estimation are successfully achieved. A single Augmented Dynamics Extended Kalman Filter (ADEKF) is configured by combining the spacecraft nonlinear attitude dynamics and quaternion kinematics with orbital mechanics. The filter design is adopted for three-axis stabilized spacecraft in low Earth orbits where the aerodynamic drag is the dominant source of disturbances in addition to the spacecraft magnetic residuals. To reduce the computational burden, another Interlaced Extended Kalman Filter (IEKF) is developed to uncouple the attitude/rate from the orbit dynamics. Both filters are implemented using the magnetometer measurements and their corresponding time derivatives. As a part of EgyptSat-1 flight scenario, detumbling and standby modes are used for performance testing of the ADEKF. The concept of local observability is applied to the basic filter and the stability is investigated by incorporating extensive Monte Carlo simulations with uniformly distributed initial conditions. The filter shows the capability of estimating the attitude better than 5 deg and rate of order 0.03 deg/s in each axis. In orbit estimation, the filter is capable of estimating the position with accuracy less than 8 km and velocity upto 5 m/s in each axis.     

基于PC/104总线的飞机电源产品综合测试系统

详细介绍了一套基于PC／104总线和虚拟仪器技术的飞机电源产品综合测试系统的功能和软硬件实现原理。阐述了测试系统的设计原理，最后结合整个系统设计介绍了在LabVIEW环境下测试系统软件的设计和实现。     

嫦娥五号平动点拓展任务轨道方案研究

中国嫦娥五号探测器成功实现月球采样返回任务,为最大限度利用任务资源,研究了利用嫦娥五号轨道器的平动点拓展任务轨道方案,设计了平动点轨道及其转移轨道.首先,给出了任务轨道设计的轨道动力学模型,包括圆型限制性三体问题模型和精确力模型.其次,基于嫦娥二号和嫦娥5T1平动点拓展任务设计经验,介绍了平动点轨道直接转移与入轨等轨道...     

基于广义相对论的轨道摄动下星间激光相位比对

针对纳米到皮米量级星间激光测距,在地心非旋转坐标系(GCRS)下,考虑卫星轨道摄动引起的广义相对论效应,建立了星间单向以及双向星间激光相位比对模型.通过仿真研究了地球主引力场范围内轨道摄动引起的广义相对论效应对星间激光相位比对误差的影响,并通过星间激光相位比对误差计算星间激光测距误差.不同轨道高度的卫星仿真结果表明,对...     

Improved orbital parameters of accreting millisecond pulsar SAX J1808.4-3658

We analyze the three outbursts of the X-ray millisecond pulsar SAX J1808.4-3658 that occurred in 1998, 2000, and 2002 observed with RXTE. With a technique based on epoch folding search we find an unique orbital solution valid over the five years of high temporal resolution data available. We revise the estimate of the orbital period, P_orb = 7249.1569(1) s and of its error, which we decrease by one order of magnitude. We also give the first constraint on the orbital period derivative, . We find that in 2002 the pulse profile shape is clearly asymmetric, showing a secondary peak at about 145° from the main pulse, which is different from the sinusoidal shape reported at the beginning of the 1998 outburst.     

X-ray timing beyond the Rossi X-ray Timing Explorer

With its ability to look at bright galactic X-ray sources with sub-millisecond time resolution, the Rossi X-ray Timing Explorer (RXTE) discovered that the X-ray emission from accreting compact stars shows quasi-periodic oscillations on the dynamical timescales of the strong field region. RXTE showed also that waveform fitting of the oscillations resulting from hot spots at the surface of rapidly rotating neutron stars constrain their masses and radii. These two breakthroughs suddenly opened up a new window on fundamental physics, by providing new insights on strong gravity and dense matter. Building upon the RXTE legacy, in the Cosmic Vision exercise, testing General Relativity in the strong field limit and constraining the equation of state of dense matter were recognized recently as key goals to be pursued in the ESA science program for the years 2015–2025. This in turn identified the need for a large (10 m² class) aperture X-ray observatory. In recognition of this need, the XEUS mission concept which has evolved into a single launch L2 formation flying mission will have a fast timing instrument in the focal plane. In this paper, I will outline the unique science that will be addressed with fast X-ray timing on XEUS.     

国内通用航空维修体系初探

针对我国通用航空产业的现状，从航空法规、机型配置和维修深度等方面分析了目前国内通用航空维修市场所存在的问题，阐述了建立通用航空维修体系的必要性，并从政策指引、大型通航企业和中小通航企业的角度对建立通用航空维修体系提出了建议。     

对接综合试验台控制系统软件快速原型开发技术

对基于快速原型设计睁对接综合试验台控制系统软件开发进行了研究。介绍了根据系统方案进行的中央控制台软件设计和模型计算机软件开发等。给出了快速原型设计,以及包括接口设计、配置管理、文档管理等软件工程化管理等关键技术。     

X射线脉冲星导航中的滤波方法分析

X射线脉冲星导航由于需要大量的观测数据来确定天体方位,因此需要较长的滤波周期(500 ～ 1000s),系统的状态方程是非线性的.若采用扩展Kalman滤波(EKF),线性化时会产生较大的高阶截断误差,且Jacobian矩阵不易精确计算,导致定轨的精度较低.文中采用非线性滤波方法- Unscented Kalman 滤...