共查询到17条相似文献,搜索用时 852 毫秒
1.
针对局部重力异常向上延拓计算复杂、耗时长的问题,该文基于泊松积分离散化的基本原理,提出一种快速的局部格网重力异常向上延拓的实用算法;并结合中国东北和青藏高原地区大地水准面的重力异常格网数据,采用该延拓方法分别计算了空中10、50、100km处的重力异常,将其与等高度的EIGEN-6C4模型结果对比分析。实验结果表明:在顾及边界效应影响的情况下,相对于EIGEN-6C4模型,中国东北和青藏高原地区重力异常向上延拓的最大均方根误差分别优于1.5和3.5mGal;在保证精度可用的前提下,计算效率可以有大幅度提高,证明了该方法解算局部重力异常向上延拓的适用性。 相似文献
2.
重力向上延拓在外部重力场逼近和航空重力测量数据质量评估中具有重要应用。本文深入分析研究了6种向上延拓计算模型的技术特点和适用条件,提出了应用超高阶位模型加地形改正、点质量方法结合移去-恢复技术实现“先向下后向上延拓”计算的实施策略,探讨了计算过程特别是前端向下延拓过程的稳定性问题。通过实际数值计算,定量评估了地形质量对不同高度向上延拓结果的影响,对比分析了不同向上延拓模型顾及地形效应的实际效果,同时对向上延拓模型计算精度进行了估计。在地形变化比较激烈的山区,地形质量对向上延拓结果的影响最大可达几十个mGal(10-5m·s-2),当计算高度为10 km时,该项影响超过3 mGal;向上延拓计算模型误差(不含数据误差影响)一般不超过1 mGal;基于超高阶位模型和地形改正信息实施向下延拓过渡的布阿桑(Poisson)积分向上延拓模型,具有计算过程简便、计算结果稳定可靠等优点。 相似文献
3.
《武汉大学学报(信息科学版)》2020,(10)
在航空重力向下延拓过程中,将重力数据中的系统误差和离散化造成的模型误差用非参数分量表达。在无外部数据的情况下,建立基于半参数核估计方法的重力向下延拓模型,为了改善泊松积分离散后的设计矩阵的病态影响,引入正则化方法,提出了综合半参数核估计和正则化方法的逆泊松积分延拓方法。基于EGM2008(earth gravity model 2008)模型计算了某地空中重力异常,采用线性项和周期项系统误差进行仿真实验,以及美国某地实测重力异常数据,验证了本文方法在改善病态性和分离系统误差方面的有效性。结果表明,本文方法在无外部数据时,能有效地分离系统误差并具有较高的精度。 相似文献
4.
CHZ-Ⅱ重力仪是首套完全国产零长弹簧原理航空重力仪,2018年4月在陕西渭南地区进行了首次飞行试验,共完成4个架次24条测线的有效飞行,标志着我国航空重力仪在自主研发的道路上又取得了长足的进步。利用飞行地区地面重力数据对CHZ-Ⅱ重力仪的测线扰动重力和格网扰动重力数据进行精度评估,其中空中测线在10 km分辨率条件下,精度达到1 mGal。采用地形辅助法对测量形成的5'测格网重力数据进行向下延拓,经延拓至地面后精度优于5 mGal,基本满足平原地区的测量需求。 相似文献
5.
目前,航空重力测量是快速获取陆地和近海区域高精度、高分辨率重力场信息的非常有效的技术手段,向下延拓则是其数据处理中的关键环节,直接影响到测量结果的进一步应用。本文在对传统最小二乘法、改进最小二乘法、Tikhonov正则化法等延拓模型进行数值分析的基础上,根据调和函数的基本特性,提出并建立了Poisson积分迭代法和改进Poisson积分迭代法延拓模型。实测航空和地面重力测量数据的试验结果表明,本文新建的Poisson积分迭代法和改进Poisson积分迭代法延拓模型精度相当,比传统最小二乘法延拓模型精度提高了15.26 mGal,比改进最小二乘法延拓模型精度提高了0.21 mGal,比Tikhonov正则化法延拓模型精度略低0.13 mGal,从而证明了本文所建模型的正确性和有效性。 相似文献
6.
针对航空重力测量受到飞机状态和气流变化等因素影响的特点和常规重复测线对比方法的缺点,该文提出了顾及平面位置纠正和高度归算的重复测线对比分析和交叉点分析方法。选取两两组合模式进行重复测线对比分析,建立多参数精度指标,采用交叉点分析,对毛乌素测区航空重力空中测线数据内符合精度进行评价。结果表明:4条重复测线的绝对平均偏差为0.01~0.95mGal,标准差为0.87~1.44mGal,两两组合对比模式在鉴别问题测线方面更有优势;在231个交叉点处,经过交叉点平差处理,均方根差值从平差前的1.6mGal减小到1.34mGal。 相似文献
7.
飞机运动加速度的测量精度是制约航空重力测量技术发展的主要障碍之一。相较于传统动态差分GPS(differential GPS,DGPS)技术,所提方法采用单站测量模式,无需布设地面基准站。首先通过相位历元间差分解得高精度历元间位移序列,然后结合泰勒一阶中心差分获得载体加速度,重点分析了卫星轨道和卫星钟差对加速度估计的影响,结果表明,不同卫星轨道产品对加速度估计影响较小,而卫星钟差采样率对加速度估计的影响很大。结合中国陕西省境内的GT-2A航空重力测量系统飞行实测数据,利用单站法解算的加速度联合重力和姿态数据解算重力扰动结果与DGPS解算的重力扰动符合较好,当滤波长度为100 s时,两者互差优于1.0 mGal。重力扰动交叉点不符值网平差后,均方根(root mean square,RMS)为1.13 mGal。与地面重力实测值比较的结果表明,所提方法与DGPS方法在精度上基本一致,说明单站法标量航空重力测量是可行的。 相似文献
8.
渤海湾航空重力及其在海域大地水准面精化中的应用 总被引:1,自引:1,他引:0
近海航空重力数据在陆海大地水准面统一中起着重要作用。近3年来,利用我国首套航空重力测量系统(CHAGS)完成了渤海湾地区近20万平方千米的5′×5′格网平均重力异常数据的获取。本文首先介绍了渤海湾地区航空重力测量的概况,给出航空重力测量数据的处理要点;然后,详细讨论了航空重力测量的精度评估方法,其中针对该区域的测线布设特点,提出了"重叠格网比较法"以评估格网平均重力异常的内符合精度。结果表明,对于5′的波长分辨率,交叉点重力异常不符值在抗差后的中误差约为1.5 mGal,重叠格网法获得的5′×5′格网平均重力异常的中误差约为1.6 mGal;5′×5′格网重力异常与卫星测高和船测重力的比较精度优于3.0mGal;由航空重力测量获得的1°×1°格网平均重力异常与GOCE卫星重力位模型的计算值相比较,其系统性差异小于0.5 mGal、中误差约为2.7 mGal。利用航空重力数据后,渤海湾区域大地水准面与16个GPS水准点的比较精度由EGM2008模型的约23 cm提高到约12 cm。 相似文献
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10.
利用泊松积分法和点质量法对澳大利亚West Arnhem Land区域的航空重力测量数据进行了精度评估,两种方法得到精度结果基本一致,评估结果表明GT-1A测量系统2′分辨率数据的测量精度优于3×10-5 m/s2,5′分辨率数据的测量精度优于2×10-5 m/s2。利用交叉点平差和泊松积分法、点质量法对渤海区域的航空重力测量进行了内部交叉点平差和外部精度评估,结果表明,内部评估精度与外部评估精度存在一定的差异,以外部评估为准则,CHAGS测量系统在渤海区域5′分辨率的航空重力数据精度优于3.5×10-5 m/s2。综合国内外试验情况分析得到,在近海区域,航空重力数据的分辨率和精度受测量仪器的性能而不同,整体上对于5′分辨率数据而言,可以达到或优于3×10-5 m/s2的精度。 相似文献
11.
M. S. Senobari 《Journal of Geodesy》2010,84(5):277-291
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. 相似文献
12.
SUN Zhongmiao XIA Zheren LI Yingchun 《地球空间信息科学学报》2007,10(3):163-167
Abstract The cross-coupling corrections for the LaCoste & Romberg airborne gravimeter are computed as a linear combination of 5 so-called cross-coupling monitors. The weight factors (coefficients) determined from marine gravity data by the factory are obviously not optimal for airborne application. These coefficients are recalibrated by minimizing the difference between airborne data and upward continued surface data (external calibration) and by minimizing the errors at line crossings (internal calibration) respectively. An integrating method to recalibrate the above-mentioned coefficients and the beam scale factor simultaneously is also presented. Experimental results show that the systemic errors in the airborne gravity anomalies can be greatly reduced by using any of the recalibrated coefficients. For example, the systemic error is reduced from 4.8 mGal to 1.8 mGal in Datong test. 相似文献
13.
Flight test results from a strapdown airborne gravity system 总被引:3,自引:0,他引:3
In June 1995, a flight test was carried out over the Rocky Mountains to assess the accuracy of airborne gravity for geoid
determination. The gravity system consisted of a strapdown inertial navigation system (INS), two GPS receivers with zero baseline
on the airplane and multiple GPS master stations on the ground, and a data logging system. To the best of our knowledge, this
was the first time that a strapdown INS has been used for airborne gravimetry. The test was designed to assess repeatability
as well as accuracy of airborne gravimetry in a highly variable gravity field. An east-west profile of 250 km across the Rocky
Mountains was chosen and four flights over the same ground track were made. The flying altitude was about 5.5km, i.e., between
2.5 and 5.0km above ground, and the average flying speed was about 430km/h. This corresponds to a spatial resolution (half
wavelength of cutoff frequency) of 5.07.0km when using filter lengths between 90 and 120s. This resolution is sufficient for
geoid determination, but may not satisfy other applications of airborne gravimetry. The evaluation of the internal and external
accuracy is based on repeated flights and comparison with upward continued ground gravity using a detailed terrain model.
Gravity results from repeated flight lines show that the standard deviation between flights is about 2mGal for a single profile
and a filter length of 120s, and about 3mGal for a filter length of 90s. The standard deviation of the difference between
airborne gravity upward continued ground gravity is about 3mGal for both filter lengths. A critical discussion of these results
and how they relate to the different transfer functions applied, is given in the paper. Two different mathematical approaches
to airborne scalar gravimetry are applied and compared, namely strapdown inertial scalar gravimetry (SISG) and rotation invariant
scalar gravimetry (RISG). Results show a significantly better performance of the SISG approach for a strapdown INS of this
accuracy class. Because of major differences in the error model of the two approaches, the RISG method can be used as an effective
reliability check of the SISG method. A spectral analysis of the residual errors of the flight profiles indicates that a relative
geoid accuracy of 23cm over distances of 200km (0.1 ppm) can be achieved by this method. Since these results present a first
data analysis, it is expected that further improvements are possible as more refined modelling is applied.
Received: 19 August 1996 / Accepted: 12 May 1997 相似文献
14.
Accurate upward continuation of gravity anomalies supports future precision, free-inertial navigation systems, since the latter
cannot by themselves sense the gravitational field and thus require appropriate gravity compensation. This compensation is
in the form of horizontal gravity components. An analysis of the model errors in upward continuation using derivatives of
the standard Pizzetti integral solution (spherical approximation) shows that discretization of the data and truncation of
the integral are the major sources of error in the predicted horizontal components of the gravity disturbance. The irregular
shape of the data boundary, even the relatively rough topography of a simulated mountainous region, has only secondary effect,
except when the data resolution is very high (small discretization error). Other errors due to spherical approximation are
even less important. The analysis excluded all measurement errors in the gravity anomaly data in order to quantify just the
model errors. Based on a consistent gravity field/topographic surface simulation, upward continuation errors in the derivatives
of the Pizzetti integral to mean altitudes of about 3,000 and 1,500 m above the mean surface ranged from less than 1 mGal
(standard deviation) to less than 2 mGal (standard deviation), respectively, in the case of 2 arcmin data resolution. Least-squares
collocation performs better than this, but may require significantly greater computational resources. 相似文献
15.
Downward continuation and geoid determination based on band-limited airborne gravity data 总被引:4,自引:3,他引:4
The downward continuation of the harmonic disturbing gravity potential, derived at flight level from discrete observations
of airborne gravity by the spherical Hotine integral, to the geoid is discussed. The initial-boundary-value approach, based
on both the direct and inverse solution to Dirichlet's problem of potential theory, is used. Evaluation of the discretized
Fredholm integral equation of the first kind and its inverse is numerically tested using synthetic airborne gravity data.
Characteristics of the synthetic gravity data correspond to typical airborne data used for geoid determination today and in
the foreseeable future: discrete gravity observations at a mean flight height of 2 to 6 km above mean sea level with minimum
spatial resolution of 2.5 arcmin and a noise level of 1.5 mGal. Numerical results for both approaches are presented and discussed.
The direct approach can successfully be used for the downward continuation of airborne potential without any numerical instabilities
associated with the inverse approach. In addition to these two-step approaches, a one-step procedure is also discussed. This
procedure is based on a direct relationship between gravity disturbances at flight level and the disturbing gravity potential
at sea level. This procedure provided the best results in terms of accuracy, stability and numerical efficiency. As a general
result, numerically stable downward continuation of airborne gravity data can be seen as another advantage of airborne gravimetry
in the field of geoid determination.
Received: 6 June 2001 / Accepted: 3 January 2002 相似文献
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经典物理大地测量学利用斯托克斯方法和莫洛金斯基方法解算大地测量边值问题并给出地球外部重力场表达,若忽略1~2 m量级的动力学海面地形,静止的平均海面可认为是大地水准面,后者是与平均海平面最为接近的重力等位面。经典理论无法求解海洋内部,即地球内部重力场问题,为解决这一局限,基于地表浅层法引入“浅层海水”的概念,“浅层海水”上下界面由平均海面高模型DTU21确定,利用牛顿积分和球谐展开算法确定了最优球谐分析迭代次数,分析了“浅层海水”厚度与积分区域半径大小的关系,确定了“浅层海水”厚度为100 m、500 m和1 000 m时的最优积分区域半径为1°,厚度4 000 m时为1.5°;评估了“浅层海水”质量法移去-恢复海洋表面重力值的精度,“浅层海水”厚度100 m、500 m、1 000 m和4 000 m的均方根误差分别为0.13 mGal、0.61 mGal、1.21 mGal和3.93 mGal,验证了该方法的可靠性。基于此理论,计算了不同厚度“浅层海水”下表面的层面重力值,得到了100 m、500 m、1 000 m和4 000 m深度处层面重力值与“浅层海水”上表面重力值差的均方根,分别为22.11 mGal、110.50 mGal、220.87 mGal和877.31 mGal。 相似文献