航空重力仪的动态检测

20 0 0年 3月 ,我们引进了国内首套 L acoste&Romberg航空重力仪。为检测其动态测量精度 ,研制了“正弦式航空重力仪检测平台”。在对该平台的设计原理作简要介绍后 ,详细讨论了检测数据的处理方法 ,然后对该航空重力仪的动态检测数据作了分析和比较。检测结果表明 ,该型仪器的动态测量精度与仪器标称精度相一致     

L＆R航空重力仪的水平加速度改正

L&R(LaCoste&Romberg)航空重力仪是我国首套航空重力测量系统的核心,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.飞行测量时,由于水平加速度的存在,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.介绍了水平加速度计算的两种基本方法,即两步法与一步法,从理论上导出了其在平台倾角较小情况下的等价性.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.通过平台倾角的谱分析,确定了预滤波尺度,即采用与平台稳定周期相当的低通滤波器进行预滤波.最后利用实测数据对此进行了验证和分析.结果表明, 利用预滤波尺度, 航空重力测量值与地面向上延拓参考值的系统差由5×10-5 m·s-2减小至0.5×10-5 m·s-2.     

LaCoste＆Romberg航空重力仪的交叉耦合改正

基于最小二乘原理．分别利用地面重力测量数据、交叉点重力异常不符值对CC（cross—coupling）监视项系数进行了重新标定，同时给出了CC监视项系数和摆杆尺度因子的联合标定方法。试验结果表明，采用新系数显著地降低了空中重力异常估值的系统误差，对于大同航空重力测量，系统误差从4．8mGal减小至1．8mGal。     

L&R航空重力仪的水平加速度改正

L&R(LaCoste&Romberg)航空重力仪是我国首套航空重力测量系统的核心,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.飞行测量时,由于水平加速度的存在,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.介绍了水平加速度计算的两种基本方法,即两步法与一步法,从理论上导出了其在平台倾角较小情况下的等价性.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.通过平台倾角的谱分析,确定了预滤波尺度,即采用与平台稳定周期相当的低通滤波器进行预滤波.最后利用实测数据对此进行了验证和分析.结果表明, 利用预滤波尺度, 航空重力测量值与地面向上延拓参考值的系统差由5×10-5 m·s-2减小至0.5×10-5 m·s-2.     

L&R航空重力仪的水平加速度改正

L&R(LaCoste&Romberg)航空重力仪是我国首套航空重力测量系统的核心,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。飞行测量时,由于水平加速度的存在,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。介绍了水平加速度计算的两种基本方法,即两步法与一步法,从理论上导出了其在平台倾角较小情况下的等价性。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。通过平台倾角的谱分析,确定了预滤波尺度,即采用与平台稳定周期相当的低通滤波器进行预滤波。最后利用实测数据对此进行了验证和分析。结果表明,利用预滤波尺度,航空重力测量值与地面向上延拓参考值的系统差由5×10-5m.s-2减小至0.5×10-5m.s-2。     

LaCoste & Romberg航空重力仪的零点漂移

概述LaCoste&Romberg(L&R)航空重力仪零点漂移的计算方法。以连续48天的实验室观测数据分析SA-1航空重力仪零点漂移的特点,以野外实测数据计算SA-1和SA-2两套航空重力仪的零点漂移。最后,简要给出航空重力测量数据处理中零点漂移的顾及方法。     

航空重力测量技术及其应用

近十几年来,航空重力测量技术的研究和应用日趋活跃,业已成为地球重力场研究中最为热门的领域之一。本文介绍了国外航空重力测量技术及其应用情况,概述了我国首套航空重力测量系统CHAGS的试验、作业和应用现状,对航空重力测量发展趋势作了展望。     

L&R航空重力仪摆杆尺度因子的确定与分析

讨论了K因子的实验确定方法，基于重力仪检测平台的检测数据和航空重力测量实测数据，分析了K因子对计算结果的影响。     

航空矢量重力测量中姿态误差的分析

本文首先给出了航空矢量重力测量的数学模型,并依此得出了扰动重力矢量的误差模型。重点研究了平台式和捷联式两种情况下姿态误差对扰动重力矢量的影响,并得到了一致的姿态指标。水平姿态误差应小于0．2″,垂直姿态误差应小于10″,对航空矢量重力测量的发展具有一定的指导意义。     

高精度海洋重力仪系统误差建模研究

导出高精度海洋重力仪系统的速度控制方程、角速度控制方程和纬度控制方程。以高精度海洋重力仪系统中平台的横倾角、纵倾角、运载体的东向速度误差、北向速度误差和运载体的纬度误差为变量,导出高精度海洋重力仪系统误差模型,并进行了系统误差仿真实验.理论分析和仿真实验表明:高精度海洋重力仪的系统误差形成过程分为误差积累、误差衰减和误差稳定三个阶段;0~1800 s是系统误差积累阶段,最大系统误差约为3.0×10-6m/s2;由于水平阻尼网络的作用,从1800~3000 s是仪系统误差衰减阶段;3000 s以后,系统误差进入稳定阶段,仿真4000 s时,系统误差约为2.246×10-6m/s2。     

Application of a spherical FFT approach in airborne gravimetry

The basic idea of this paper is to modifyPoisson's integral for harmonic downward continuation into a convolution formula in the space domain. In this manner, the Fast Fourier Transform can be applied. The method is applied to airborne gravimetry, motivated especially by the Greenland survey. The accuracy of data continuation from the flight-level to the ground is analysed. In particular, the influence of latitudinal extension is investigated, since the introduced convolution formula is exact only for the mid-parallel of the analysed area. The results obtained justify the conclusion that the introduced method is applicable to processing of real data. Extended quadratic areas (up to 2500km × 2500km) in equatorial areas and up to 500km × 500km in regions with latitudes about 75°) can effectively be processed in one single procedure.     

似大地水准面的定义及在空中测量中涉及的问题

本文讨论了高程异常和似大地水准面的定义以及高程异常随空间位置的变化,提出了将似大地水准面称为正常高系统的高程基准面的不恰当性,给出了由地面测量至空中点几何高差确定空中点正常高的改正方法。其目的主要是针对当前已经扩展到了空中的测量,引导正确地认识正常高系统的基本问题。     

New results in airborne vector gravimetry using strapdown INS/DGPS

A method for airborne vector gravimetry has been developed. The method is based on developing the error dynamics equations of the INS in the inertial frame where the INS system errors are estimated in a wave estimator using inertial GPS position as update. Then using the error-corrected INS acceleration and the GPS acceleration in the inertial frame, the gravity disturbance vector is extracted. In the paper, the focus is on the improvement of accuracy for the horizontal components of the airborne gravity vector. This is achieved by using a decoupled model in the wave estimator and decorrelating the gravity disturbance from the INS system errors through the estimation process. The results of this method on the real strapdown INS/DGPS data are promising. The internal accuracy of the horizontal components of the estimated gravity disturbance for repeated airborne lines is comparable with the accuracy of the down component and is about 4–8 mGal. Better accuracy (2–4 mGal) is achieved after applying a wave-number correlation filter (WCF) to the parallel lines of the estimated airborne gravity disturbances.     

Using radial basis functions in airborne gravimetry for local geoid improvement

Radial basis functions (RBFs) have been used extensively in satellite geodetic applications. However, to the author’s knowledge, their role in processing and modeling airborne gravity data has not yet been fully advocated or extensively investigated in detail. Compared with satellite missions, the airborne data are more suitable for these kinds of localized basis functions especially considering the following facts: (1) Unlike the satellite missions that can provide global or near global data coverage, airborne gravity data are usually geographically limited. (2) It is also band limited in the frequency domain. (3) It is straightforward to formulate the RBF observation equations from an airborne gravimetric system. In this study, a set of band-limited RBF is developed to model and downward continue the airborne gravity data for local geoid improvement. First, EIGEN6c4 coefficients are used to simulate a harmonic field to test the performances of RBF on various sampling, noise, and flight height levels, in order to gain certain guidelines for processing the real data. Here, the RBF method not only successfully recovers the harmonic field but also presents filtering properties due to its particular design in the frequency domain. Next, the software was tested for the GSVS14 (Geoid Slope Validation Survey 2014) area in Iowa as well as for the area around Puerto Rico and the US Virgin Islands by use of the real airborne gravity data from the Gravity for the Redefinition of the American Vertical Datum (GRAV-D) project. By fully utilizing the three-dimensional correlation information among the flight tracks, the RBF can also be used as a data cleaning tool for airborne gravity data adjustment and cleaning. This property is further extended to surface gravity data cleaning, where conventional approaches have various limitations. All the related numerical results clearly show the importance and contribution of the use of the RBF for high- resolution local gravity field modeling.     

Strapdown INS/DGPS airborne gravimetry tests in the Gulf of Mexico

Combining data from a Strapdown Inertial Navigation System and a Differential Global Positioning System (SINS/DGPS) has shown great promise in estimating gravity on moving platforms. Previous studies on a ground-vehicle system obtained 1–3 mGal precision with 2 km spatial resolution. High-accuracy Inertial Measurement Units (IMU) and cm-level positioning solutions are very important in obtaining mGal-level gravity disturbance estimates. However, these ideal configurations are not always available or achievable. Because the noise level in the SINS/DGPS gravimetric system generally decreases with an increase of speed and altitude of the platform, the stringent constraints on the IMU and GPS may be relieved in the airborne scenario. This paper presents an investigation of one navigation-grade and one tactical-grade IMU for the possibility of low-cost INS/GPS airborne gravimetry. We use the data collected during the Gravity-Lidar Study of 2006 (GLS06), which contains aerogravity, GPS, and INS along the northern coastline of the Gulf of Mexico. The gravity disturbance estimates from the navigation-grade IMU show 0.5–3.2 mGal precision compared with the onboard gravimeter’s measurements and better than 3 mGal precision compared with the upward continued surface control data. Due to relatively large (240 s) smoothing window, the results have about 34 km along-track resolution. But the gravity estimates from the tactical-grade IMU have much poorer precisions. Nonetheless, useful contributions from the tactical-grade IMU could be extracted for longer wavelengths.     

补偿海空重力测量动态效应剩余影响的通用模型

针对目前作业过程中普遍存在的测量动态环境效应剩余影响问题,在深入分析海空重力测量误差源形成机理及其变化特性基础上,提出了一种适用于补偿各类海空重力仪动态效应剩余影响的通用模型;研究探讨了通用模型形式优选和模型参数估计问题,将基于信息论的Akaike信息量准则引入通用模型表达式的优选过程,提出应用互相关分析方法对模型参数进行估计,在双重约束下构建了补偿动态效应剩余影响的优化模型。使用典型动态环境下的海面重力观测数据对该方法的有效性进行了验证,结果显示,海洋重力测量成果内符合精度从原先的±9.35×10^-5 m/s²大幅提升到±1.01×10^-5 m/s²,充分体现了本文方法和模型对消除高动态测量环境效应影响的优良特性。     

低空机载LiDAR点云定位误差分析

低空机载LiDAR因其系统的复杂性,点云定位精度受很多系统误差影响。为了研究改善点云定位精度的方法,文中根据LiDAR定位误差模型综合分析航高、扫描角、IMU姿态角、姿态角误差等对点云定位误差的影响,并根据误差影响规律分析得出不同地形测图比例尺对飞行参数的要求。通过长江中下游实测地区作业验证,建议设置飞行参数得到的点云定位精度符合精度要求。