Comparison of Kuqa foreland basin with Persian Gulf Basin in salt tectonics

Compared Kuqa foreland basin with Persian Gulf Basin in development of salt layers, salt tectonics, and the relation between salt tectonics and hydrocarbon, it is concluded that the salt diapirs are relative to hydrocarbon. Searching salt diapirs and related traps in Kuqa foreland basin is important. The forming mechanism of salt tectonic in Kuqa foreland basin is different from that of Hormuz Series, but similar to that of Lower Fars Series/Gachsaran Formation. Inspired by the role of salt tectonics of Lower Fars Series/Gachsaran Formation in hydrocarbon accumulation, the authors considered that the exploration below salt layer should be enforced, and the traps below salt layer in the southern part of the Kuqa foreland basin would be found where salt layer is thicker. On the contrary, the traps should be found both above and below the salt layer in front of the northern mountain where salt layer is thin. The Triassic and Jurassic source rocks are rich in this area with great exploration prospective.     

基于离散小波变换的数字水印技术

提出了一种基于小波分析的简单有效的数字水印嵌入和盲检测的算法。先将嵌入的水印信息加密，然后将加密后的水印信息嵌到相应DWT系数的有效嵌入位中，并使用适当的保真技术，减小图像因嵌入水印引起的失真。通过实验验证，该算法在对嵌入水印后的图像进行有损压缩、剪切、污染、添加各种噪声等处理后，提取出的水印仍表现出了较好的鲁棒性。     

GLONASS卫星位置的动力学改进算法

为了减弱由于广播星历拟合引起的误差,本文提出了一种基于动力学轨道改进的GLONASS卫星位置算法。该算法仅采用GLONASS广播星历信息就能够提高GLONASS卫星位置坐标的计算精度。算例表明,该方法能够有效减弱GLONASS卫星广播星历的拟合误差,卫星位置的精度损失从0.5m降到mm级;外推2-3h,精度损失也仅在cm级水平。     

一种结合UKF与TLS的GPS机动跟踪算法

在GPS接收机产生机动时,运动模型的不匹配会给跟踪算法带来性能损失。本文提出一种机动检测、Unscented Kalman Filter(UKF)以及总体最小二乘(Total Least Square,TLS)相结合的解算方法用于接收机机动的GPS跟踪解算。首先,通过机动检测算法对目标的机动性进行判别,当目标机动较小时,利用UKF的最优检测性能进行跟踪,而当目标机动较大时,结合TLS的强跟踪性能,采用TLS和UKF联合进行跟踪。从而,在不增加方程维数的情况下,实现机动目标的实时、快速跟踪。仿真结果表明该方法对机动目标具有良好的跟踪性能。     

Initial results of centralized autonomous orbit determination of the new-generation BDS satellites with inter-satellite link measurements

Autonomous orbit determination is the ability of navigation satellites to estimate the orbit parameters on-board using inter-satellite link (ISL) measurements. This study mainly focuses on data processing of the ISL measurements as a new measurement type and its application on the centralized autonomous orbit determination of the new-generation Beidou navigation satellite system satellites for the first time. The ISL measurements are dual one-way measurements that follow a time division multiple access (TDMA) structure. The ranging error of the ISL measurements is less than 0.25 ns. This paper proposes a derivation approach to the satellite clock offsets and the geometric distances from TDMA dual one-way measurements without a loss of accuracy. The derived clock offsets are used for time synchronization, and the derived geometry distances are used for autonomous orbit determination. The clock offsets from the ISL measurements are consistent with the L-band two-way satellite, and time–frequency transfer clock measurements and the detrended residuals vary within 0.5 ns. The centralized autonomous orbit determination is conducted in a batch mode on a ground-capable server for the feasibility study. Constant hardware delays are present in the geometric distances and become the largest source of error in the autonomous orbit determination. Therefore, the hardware delays are estimated simultaneously with the satellite orbits. To avoid uncertainties in the constellation orientation, a ground anchor station that “observes” the satellites with on-board ISL payloads is introduced into the orbit determination. The root-mean-square values of orbit determination residuals are within 10.0 cm, and the standard deviation of the estimated ISL hardware delays is within 0.2 ns. The accuracy of the autonomous orbits is evaluated by analysis of overlap comparison and the satellite laser ranging (SLR) residuals and is compared with the accuracy of the L-band orbits. The results indicate that the radial overlap differences between the autonomous orbits are less than 15.0 cm for the inclined geosynchronous orbit (IGSO) satellites and less than 10.0 cm for the MEO satellites. The SLR residuals are approximately 15.0 cm for the IGSO satellites and approximately 10.0 cm for the MEO satellites, representing an improvement over the L-band orbits.     

Three-frequency BDS precise point positioning ambiguity resolution based on raw observables

All BeiDou navigation satellite system (BDS) satellites are transmitting signals on three frequencies, which brings new opportunity and challenges for high-accuracy precise point positioning (PPP) with ambiguity resolution (AR). This paper proposes an effective uncalibrated phase delay (UPD) estimation and AR strategy which is based on a raw PPP model. First, triple-frequency raw PPP models are developed. The observation model and stochastic model are designed and extended to accommodate the third frequency. Then, the UPD is parameterized in raw frequency form while estimating with the high-precision and low-noise integer linear combination of float ambiguity which are derived by ambiguity decorrelation. Third, with UPD corrected, the LAMBDA method is used for resolving full or partial ambiguities which can be fixed. This method can be easily and flexibly extended for dual-, triple- or even more frequency. To verify the effectiveness and performance of triple-frequency PPP AR, tests with real BDS data from 90 stations lasting for 21 days were performed in static mode. Data were processed with three strategies: BDS triple-frequency ambiguity-float PPP, BDS triple-frequency PPP with dual-frequency (B1/B2) and three-frequency AR, respectively. Numerous experiment results showed that compared with the ambiguity-float solution, the performance in terms of convergence time and positioning biases can be significantly improved by AR. Among three groups of solutions, the triple-frequency PPP AR achieved the best performance. Compared with dual-frequency AR, additional the third frequency could apparently improve the position estimations during the initialization phase and under constraint environments when the dual-frequency PPP AR is limited by few satellite numbers.     

星载激光光斑影像质心自动提取方法

激光光斑影像的质心提取是卫星激光测高数据处理中的重要环节,对于获得精确的激光指向角有重要的意义。本文总结了灰度重心法、高斯拟合法以及椭圆拟合法3种常用的质心提取方法,在比较其优缺点之后结合高斯曲面拟合法和椭圆拟合法,提出了一种基于高斯阈值的椭圆拟合方法,针对仿真数据进行试验,有较好的精度结果。采用GLAS（geoscience laser altimeter system）的实际激光光斑影像LPA（laser profile array）数据进行试验,发现LPA光斑质心位置变化周期约为1.5 h,幅度最大可达2~3个像素,对应激光指向角变化约9",说明在轨监视激光质心位置变化对于提高激光指向角测量精度非常必要。相关结论可为后续国产卫星激光测高仪足印影像处理提供参考。     

北斗高精度长弧历书模型设计

历书参数可同时用于辅助常规导航和自主导航的信号捕获。延长历书参数的有效期不但可以使地面接收机启动时充分利用历书数据,对于基于星间链路观测的自主导航,历书参数的有效期还决定了地面注入历书的频度和占用的星上存储资源。通过对北斗3类导航卫星主要摄动力及其对轨道根数的长期项和长周期项的影响分析,设计了以6个轨道根数和5个摄动参数为播发参数的历书拟合模型。以一个自主运行周期90 d为时间尺度,对北斗在轨卫星进行了长弧段历书拟合试验,并同时分析了卫星位置和速度的拟合精度。结果表明新的历书拟合模型提高了历书拟合的精度,尤其对于地球静止轨道和倾斜地球同步轨道卫星,拟合精度提高显著。对于GEO和IGSO卫星,位置拟合误差大约从200 km降低至十几千米甚至几千米,速度拟合误差大约从15 m/s降低至0.6 m/s,新方法拟合精度提高了约20~30倍;对于中圆地球轨道卫星,无论采用哪种历书模型,位置拟合误差都在5 km左右,速度拟合误差都在0.6 m/s左右,新方法拟合精度提高约15%。针对星间链路卫星10 km位置误差上限的使用需求,对比了新老历书模型的拟合弧长,常规模型最大拟合弧长约为14 d,而新历书模型的最大拟合弧长可延长至45 d,新历书模型延长了历书使用期限,优化了北斗历书模型设计。     

自动化多面函数GPS高程拟合在既有铁路中的应用

大量的既有铁路面临改造从而提高铁路运输效率。相比传统的全站仪测量方法,利用GPS技术进行控制测量能够极大地提高效率。针对GPS控制测量在既有铁路中控制网建设中的应用,提出一种新的自动化多面函数模型用于既有铁路的GPS高程拟合。结果表明,自动化多面函数能够实现结点和结点个数自动选取,提高高程拟合精度。既有铁路高程拟合实例表明,自动化多面函数GPS高程拟合模型精度明显优于二次曲面函数模型。     

一种基于高通滤波的主成分分析影像融合方法

针对主成分分析(PCA)变换影像融合过程中变量降维信息损失较多的问题,提出了一种基于高通滤波的主成分分析(PCA)变换融合方法。该方法首先对高分辨率影像在高通滤波模块上进行卷积运算,然后将滤波过后的影像与主成分变换后的第一主分量进行直方图匹配和加权平均运算;最后用直方图匹配过的高分辨率影像代替第一主分量与其他分量经K-L逆变换得到融合结果。选取北京二号卫星影像进行试验,通过将PCA变换和HPF融合结果进行对比评价,结果表明了该方法很好地提高了影像的空间细节信息与光谱保持能力,实验结果将为后续高分系列卫星影像处理提供支持。