附有物理量和气象条件约束的光学卫星国土观测有效覆盖率评估

传统光学卫星国土观测覆盖评估建立在卫星对地理想覆盖的基础上,并未考虑卫星存储、星地数据传输、观测时长等物理量及观测区域气象因素对于覆盖性能的影响。本文针对光学遥感卫星的国土观测需求.建立国土观测有效覆盖能力评估指标体系,根据卫星数据存储能力、星地数据传输能力、卫星单圈最大观测时长、卫星观测太阳高度角等性能参数,提出了基于物理性能约束下的有效覆盖计算方法。根据气象台站历年气象数据,提出了气象约束因子的计算方法。综合考虑卫星物理性能约束与观测区域气象约束,计算光学遥感卫星对地观测有效覆盖能力。最后根据专家设计的光学遥感卫星国土观测有效覆盖能力评估指标权重,利用层次分析法(AHP)评估光学遥感卫星系统对于国土观测的需求满足程度。试验结果表明,本文方法对于国土观测有效覆盖的估算和评价结果更加精确,更接近于国土观测的实际应用需求,为对地观测有效覆盖能力评估提供了一种更为精确的可行方案。     

一种状态区间取值修正的灰色-马尔科夫链预测模型研究

提出了一种对灰色-马尔科夫链预测模型的状态区间取值修正方法.考虑实测值在状态区间中的位置分布情况作为先验知识,对状态区间的端点重新定权,修正预测值在状态区间中的取值,从而获得更高精度的预测结果.结合某建筑物的实测沉降数据,与原始GM(1,1)、残差修正G M(1,1)、灰色-马尔科夫链预测模型进行对比,结果表明:本文预...     

机载激光雷达数据采集过程初探

机载激光雷达已成为快速、精确、高密度采集地形数据的有效手段,尤其在高速公路等范围狭长的区域体现明显.本文涵盖了数据采集和数据预处理等在外业采集时的关键技术,首先探讨了数据采集前的准备工作,包括检校场的选择、航线的设计、控制点的布设等重要步骤;然后说明了数据采集中的测量工作;最后讨论了数据检查工作,包括航线和激光数据的生...     

航空重力测量的空中数据处理与分析

针对航空重力测量的原始扰动数据,本文介绍了数据处理的一般流程,内容包括原始数据检查、零点漂移校正、平均高程面归算、交叉点搜寻、内符合精度评价、离散数据的格网化等方面,详细说明了每一步数据处理的理论模型,并通过工程实例对计算结果进行了讨论和分析,为今后开展大规模航空重力测量业务作出一定的尝试和探索.     

基于图形分割的面状符号自动填充算法

针对现有制图软件在面状符号填充方面存在的符号缺失、压盖等问题,提出了一种基于图形分割的面状符号自动填充算法.该算法通过计算面的骨架线,对复杂面进行分解,判断分解后的简单面的形状,分别赋予不同的制图表达规则,实现面状符号的自动填充.结果表明,该算法可以有效实现狭长以及包含狭长分支的不规则图形的合理填充,有效解决了填充符号...     

厦门市地名专题数据更新与采集的技术实现

地名专题数据作为基础地理信息的关键因素,是任何与位置相关的信息的最本质支撑,是以大数据为中心的知识信息时代最根本的经济保障。针对厦门市地名专题数据更新与采集技术实现问题,提出一套科学的方法,并对其具体实施步骤进行详细分析,形成了地名专题数据更新与采集的作业流程,以此来为今后地名专题数据的更新与采集提供一定的参考依据,从而进一步促进我国城市建设的可持续发展。     

轻小型惯性稳定平台位置环协同通信控制方法

针对轻小型航空遥感系统对姿态大机动的快响应需求,设计了一种轻量型惯性稳定平台位置环协同通信与姿态超限快响应控制策略,将位置环反馈回路设计为两种可切换工作模式。伺服模式下,参考位置姿态系统的输出,通过设计二者协同通信,保证稳定平台对飞行姿态及扰动的实时隔离;编码器实时监测框架间相对角位置,超限位且载荷视轴与垂直方向误差较大时切换模式。超限快速回复模式下,以编码器值为位置环反馈量,使用大增益将平台由超限位置迅速调整到最大限定位置,并实时监测POS值,在载荷视轴位置误差较小时返回伺服模式。实验表明,该方法可靠、有效实现了稳定平台与位置传感器的高精度实时通信与控制。     

A modified mix-differenced approach for estimating multi-GNSS real-time satellite clock offsets

A modified mixed-differenced approach for estimating multi-GNSS real-time clock offsets is presented. This approach, as compared to the earlier presented mixed-differenced approach which uses epoch-differenced and undifferenced observations, further adds a satellite-differenced process. The proposed approach, based on real-time orbit products and a mix of epoch-differenced and satellite-differenced observations to estimate only satellite clock offsets and tropospheric zenith wet delays, has fewer estimated parameters than other approaches, and thus its implementing procedure is efficient and can be performed and extended easily. To obtain high accuracy, the approach involves three steps. First, the high-accuracy tropospheric zenith wet delay of each station is estimated using mixed-differenced carrier phase observations. Second, satellite clock offset changes between adjacent epochs are estimated using also mixed-differenced carrier phase observations. Third, the satellite clock offsets at the initial epoch are estimated using satellite-differenced pseudorange observations. Finally, the initial epoch clock results and clock offset changes are concatenated to obtain the clock results of the current epoch. To validate the real-time satellite clock results, multi-GNSS post-processing clock products from IGS ACs were selected for comparison. From the comparison, the standard deviations of the GPS, GLONASS, BeiDou and Galileo systems clock results are approximately 0.1–0.4 ns, except for the BeiDou GEO satellites. The root mean squares are about 0.4–2.3 ns, which are similar to those of other international real-time products. When the clock estimates were assessed based on a pseudo-kinematic PPP procedure, the positioning accuracies in the East, North and Up components reach 5.6, 5.5 and 7.6 cm, respectively, which meet the centimeter level and are comparable to the application of other products.     

Estimating satellite phase fractional cycle biases based on Kalman filter

Phase fractional cycle biases (FCBs) originating from satellites and receivers destroy the integer nature of PPP carrier phase ambiguities. To achieve integer ambiguity resolution of PPP, FCBs of satellites are required. In former work, least squares methods are commonly adopted to isolate FCBs from a network of reference stations. However, it can be extremely time consuming concerning the large number of observations from hundreds of stations and thousands of epochs. In addition, iterations are required to deal with the one-cycle inconsistency among FCB measurements. We propose to estimate the FCB based on a Kalman filter. The large number of observations are handled epoch by epoch, which significantly reduces the dimension of the involved matrix and accelerates the computation. In addition, it is also suitable for real-time applications. As for the one-cycle inconsistency, a pre-elimination method is developed to avoid iterations and posterior adjustments. A globally distributed network consisting of about 200 IGS stations is selected to determine the GPS satellite FCBs. Observations recorded from DoY 52 to 61 in 2016 are processed to verify the proposed approach. The RMS of wide lane (WL) posterior residuals is 0.09 cycles while that of the narrow lane (NL) is about 0.05 cycles, which indicates a good internal accuracy. The estimated WL FCBs also have a good consistency with existing WL FCB products (e.g., CNES-GRG, WHU-SGG). The RMS of differences with respect to GRG and SGG products are 0.03 and 0.05 cycles. For satellite NL FCB estimates, 97.9% of the differences with respect to SGG products are within ±?0.1 cycles. The RMS of the difference is 0.05 cycles. These results prove the efficiency of the proposed approach.     

First photometric study of the eclipsing binary PS Persei

CCD photometric observations of the eclipsing binary PS Persei (PS Per) were obtained on two consecutive days in 2009.The 2003 version of the WilsonDevinney code was used to analyze the first complete light curves in the V and R bands.It is found that PS Per is a short-period Algol-type binary with the less massive component completely filling its inner critical Roche lobe.The mass ratio of q=0.518 and the orbital inclination of i=89.86° are obtained.In addition,based on all available times of primary light...