Analysis of systematic error influences on accuracy of airborne laser scanning altimetry

The error sources related to the laser rangefinder, GPS and INS are analyzed in details. Several coordinates systems used in airborne laser scanning are set up, and then the basic formula of system is given.This paper emphasizes on discussing the kinematic offset correction between GPS antenna phase center and laser fired point. And kinematic time delay influence on laser footprint position, the ranging errors, positioning errors, attitude errors and integration errors of the system are also explored. Finally, the result shows that thekinematic time delay can be neglected as compared with other error sources. The accuracy of the coordinates is not only influenced by the amplitude of the error, but also controlled by the operation parameters such as flight height, scanning angle amplitude and attitude magnitude of the platform.     

GPS动态定位数据处理模型的比较研究

The characteristics of three GPS kinematic data processing models, Least Squares （LS）, Kalman filtering and filtering are discussed and their advantages and disadvantages are compared. With observational data and pertinent data processing software, the applicable condition, context and effect of the three models are experimented. Results show that when the mobile platform is in uniform motion, the accuracy of the three models are almost equal; when the mobile platform is in stochastic acceleration, the accuracy of H∞ filtering model is superior to that of LS, while that of Kalman filtering is the worst.     

Rotation of the Earth as a Triaxial Rigid Body

The Earth is taken as a triaxial rigid body, which rotates freely in the Euclidian space. The starting equations are the Euler dynamic equations, with A smaller than B and B smaller than C. The Euler equations are solved, and the numerical results are provided. In the calculations, the following parameters are used: (C-B)/A=0.003 273 53; (B-A)/C=0.000 021 96; (C-A)/B=0.003 295 49, and the mean angular velocity of the Earth's rotation, ω =0.000 072 921 15 rad/s. Calculations show that, besides the self-rotation of the Earth and the free Euler procession of its rotation, there exists the free nutation: the nutation angle, or the angle between the Earth's momentary rotation axis and the mean axis that periodically change with time. The free nutation is investigated.     

Antarctic Traverses from Zhongshan Station to Dome—A and the Result Analysis for the GPS Points along the Expedition Route

Some GPS points were set up and occupied and reoccupied along the traverse route from Zhongshan Station to Dome-A.The result analysis for the GPS data processed by GAMIT/GLOBK package was presented in this paper.It was indicated that the ice along the traverse route flowed with an 8-25 m/a velocity to the northwest in the last three years,which was the direction of the edge of the ice sheet.The maximum horizontal flow velocity is about 100 m/a.Moreove,due to the ice flow,a 0.2-1 m/a sedimentation rate is achieved.finally,a 1-5m/a^2 horizontal acceleration is achieved from the GPS data of the three different stages.     

Separation Problem in Satellite Gravimetry

The problem of separating gravitation from inertia is discussed in very general sense, and the conclusion is positive: man can separate gravitation from inertia, if various observation techniques are applied for. The accelerometer's position problem in satellite gravimetry is investigated, and the additional acceleration effect due to the position error of an instrument as well as the difference between the mass center and the gravity center is explored.     

Correction on Effect of Earth＇s Oblateness in Inversion of GPS Occultation Data

By using observed CHAMP orbit ephemeredes and MSISE-90 dry air model and regarding the earth as a sphere and an ellipsoid respectively, phase delays are simulated and the simulated data are retrieved under different schemes. The comparison between the inverted temperature profiles and the model temperature profiles shows that by inverting observed data, we will get temperature results with large errors if the effect of Earth＇s oblateness is omitted. The correction method is proved to be effective because the temperature errors decreased obviously with this method.     

Rank-Defect Adjustment Model for Survey-Line Systematic Errors in Marine Survey Net

In this paper,the structure of systematic and random errors in marine survey net are discussed in detail and the adjustment method for observations of marine survey net is studied,in which the rank-defect haracteristic is discovered first up to now.On the basis of the survey-line systematic error model,the formulae of the rank-defect adjustment model are deduced according to modern adjustment theory.An examle of calculations with really observed data is carried out to demonstrate the efficiency of this adjustment model.Moreover,it is proved that the semi-systematic error correction method used at present in marine gravimetry in China is a special case of the adjustment model presented in this paper.     

Measurement of similarity for spatial directions between areal objects

Similarity for spatial directions plays an important role in GIS. In this paper, the conventional approaches are analyzed. Based on raster data areal objects, the authors propose two new methods for measuring similarity among spatial directions. One is to measure the similarity among spatial directions based on the features of raster data and the changes of distances between spatial objects, the other is to measure the similarity among spatial directions according to the variation of each raster cell centroid angle. The two methods overcome the complexity of measuring similarity among spatial directions with direction matrix model and solve the limitation of small changes in direction. The two methods are simple and have broader applicability.     

Crustal Movement Patterns of China Continent Measured by GPS

This paper uses multiquadric equations interpolation to establish a widely covered and valuable speed field model of China, with which the horizontal crustal movement patterns are obtained. The present-day vertical crustal movement velocity image of China is also expressed by GPS observations, from which we can know the vertical crustal movement patterns.     

Integrated Navigation System and Experiment of a Low-Cost and Low-Accuracy SINS/GPS

When SINS (strap-down inertial navigation system) is combined with GPS, the observability of the course angle is weak. Although the course angle error is improved to some extent through Kalman filtering, the course angle still assumes a divergent trend. This trend is aggravated further when using low-cost and low-accuracy SINS. In order to restrain this trend, a method that uses AHRS to substitute for SINS course angle information is put forward aimed at the hardware component characteristic of the low-cost and low-accuracy SINS including AHRS (attitude and heading reference system) and IMU (inertial measurement unit). Real static and dynamic experiments show that the method can restrain the divergent trend of the navigation system angle effectively, and the positioning accuracy is high.     

Calculation and spectra analysis of horizontal acceleration correction (HACC) for airborne gravimetry

On the basis of a sinusoidal model of the disturbed horizontal acceleration, the spectrum characteristics of misaligned angle and horizontal acceleration correction are analyzed. In an airborne gravimetry test, the misaligned angle of platform and horizontal acceleration correction are calculated. They are 5′ and 3 mGal, respectively, when the flight is stable.     

航空重力测量中水平加速度改正的计算与频域分析

基于扰动水平加速度的正弦运动模型,对平台失准角和水平加速度改正的频谱特性进行了分析。利用某航空重力测量试验的实测数据,计算了平台失准角和水平加速度改正。     

航空重力测量的偏心改正

导出了航空重力测量偏心改正的实用计算公式 ,利用某航空重力测量实测数据 ,计算了位置、速度和加速度的偏心改正 ,并对垂直加速度、厄特弗斯改正、水平加速度改正和空间改正的偏心影响进行了详细分析 ,讨论了偏心改正对偏心距、姿态角的测定精度要求。     

高精度海洋重力测量中AIRSEA SystemⅡ的水平加速度改正

AIRSEA SystemⅡ已应用于我国的海洋重力测量,它主要由高精度的垂直加速度计和稳定平台组成。前者用于测量总加速度,后者使加速度计保持精确的垂直指向。海洋重力测量时,由于测量船水平加速度的存在,稳定平台难以精确维持水平从而使加速度计偏离正确指向,由此产生了水平加速度改正。为了提高测量精度,给出水平加速度改正计算的两种方法,即两步法和一步法。为有效地减弱因水平加速度改正不完善产生的系统性误差,提出了水平加速度改正的预滤波方法。最后利用中沙大环礁实测数据对此改正方法进行了验证和分析。     

一种改进的航空重力测量数据处理方法

目前的航空标量重力测量系统主要是在当地坐标系下求解重力垂向分量,该方法涉及厄特弗斯改正,却没有考虑垂线偏差的影响。改进方法在准惯性坐标系下求解重力观测量,给出了一个计算重力值的改进公式,避免了经典方法中的近似处理,从理论上完善了航空重力测量数据处理方法。实例验证了改进方法的正确性,并显示经典方法中的近似处理在实验区域内产生了亚mGal级的误差,这个误差在利用1/60 s以下的截断频率进行低通滤波后基本可以忽略。除了理论上对经典方法的改进,改进方法还提供了确定扰动重力水平分量的公式,经过细致的数据处理后其精度可达mGal级。     

利用B样条确定航空重力载体加速度的方法研究

介绍了B样条最小二乘法的基本原理,利用3阶B样条最小二乘法给出了包含拟合、数值微分、平滑等功能的计算方案。利用该计算方案对航空重力测量的GPS速度数据以及构造的模拟速度数据进行处理得到平滑后的加速度值。经分析,该计算方案能够简捷地去除高频噪声影响,有着良好的平滑效果。     

航空重力测量中垂直加速度确定方法的比较

垂直加速度是航空重力测量的重要改正项之一。文中概述了利用GPS确定加速度的基本方法，从理论上分析了GPS确定垂直加速度的精度，并利用航空重力测量实测数据，比较分析了惯常使用的3种垂直加速度确定方法．得出了若干初步结论。     

MATLAB中实现联合测站平差自动化

水平角观测中,分组观测方向值后要进行联合测站平差。当观测组数或联测共同方向多于两个时,只能采用条件平差法,建立条件方程式后,解法方程得出各个方向值的改正数。采用MATLAB语言编制的测站平差程序,实现了读取数据、搜索共同方向、建立条件方程、解算改正数、首方向归0并同一和标准格式输出整个流程的自动化。     

全站仪测量过程中仪器高改正问题分析

全站仪,即全站型电子速测仪（Electronic Total Station）。它是一种集光、机、电为一体的高技术测量仪器,是集水平角、垂直角、距离（斜距、平距）、高差测量功能于一体的测绘仪器系统。因其一次安置仪器就可完成该测站上全部测量工作,所以称之为全站仪,并广泛用于地上大型建筑、地下隧道施工等精密工程测量、变形监...     

影响机载激光扫描测高精度的系统误差分析

简要介绍了机载激光扫描测高技术的系统组成和发展现状。通过坐标转换技术建立起机载激光扫描对地定位的基本几何关系,并从这些几何关系出发,着重分析了动态偏心改正及动态时效误差对机载激光测高精度的影响,对不同的误差源如何影响定位结果的精度进行了讨论,最后给出模拟计算结果,得出了一些有益的结论。