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1.
For the high-resolution airborne synthetic aperture radar (SAR) stereo geolocation application, the final geolocation accuracy is influenced by various error parameter sources. In this paper, an airborne SAR stereo geolocation parameter error model, involving the parameter errors derived from the navigation system on the flight platform, has been put forward. Moreover, a kind of near-direct method for modeling and sensitivity analysis of navigation parameter errors is also given. This method directly uses the ground reference to calculate the covariance matrix relationship between the parameter errors and the eventual geolocation errors for ground target points. In addition, utilizing true flight track parameters’ errors, this paper gave a verification of the method and a corresponding sensitivity analysis for airborne SAR stereo geolocation model and proved its efficiency. 相似文献
2.
结合距离-多普勒模型，推导了SAR（synthetic aperture radar）影像定向中像点坐标粗差对误差方程的影响，分析了像点坐标粗差探测的必要性和难点；依据粗差的拟准检定法，针对SAR影像定向中的像点坐标粗差检定问题，设计了具体的解算流程和策略，首次将粗差的拟准检定法运用到机载SAR影像定向中。并分别利用模拟和实测数据进行了系统性的实验，结果表明，该方法不仅能够准确探测出多个粗差的位置，而且能够估计出粗差的大小。与SAR影像定向通常采用的最小二乘方法相比，该方法能够明显提高SAR影像定向参数的解算精度以及后续的立体定位精度，对于修复受粗差影响的SAR影像数据具有重要意义。 相似文献
3.
融合升降轨的极化干涉SAR三层模型植被高度反演方法 总被引：2，自引：0，他引：2
森林参数的获取不仅可以估算地表生物量和林下地形,还有助于研究全球碳循环和分析全球气候变化。极化干涉SAR植被参数反演算法一般是基于随机地体两层模型(RVoG),但是当实际植被有着冠层、树干层和地表层的明显三层结构时,植被参数反演精度就会变差;另外,由于机载SAR系统数据的近距远距垂直向波数差异较大,导致试验结果存在着由其引起的系统误差。针对这两个问题,本文提出了一种融合升降轨的极化干涉SAR三层模型植被参数反演方法。该方法首先采用三层植被RVoG模型修正微波在穿透植被时的散射过程;然后采用融合升降轨道数据的方式削弱其系统误差;最后,采用非线性迭代平差的反演算法来进行植被高度反演。为了验证该方法的有效性,采用了德国宇航局DLR提供的BioSAR2008项目的两景升轨及两景降轨E-SAR P波段全极化SAR数据进行试验,并采用3组反演策略进行比较分析。结果表明,三层植被模型能够更好地描述植被散射过程;同时,新方法有效降低了由垂直向波数引起的系统误差,提高了树高反演精度。 相似文献
4.
TerraSAR-X (TSX) can acquire high-resolution SAR images and due to its high orbit precision as well as its ability to acquire data from different off-nadir viewing angles, the high-precision stereo geolocation can be obtained. In this study, we investigate the absolute geolocation accuracy of TSX high-resolution images in Wuhan, China. We present a direct stereo SAR geolocation method and analyze the 2D and 3D geoposition accuracy of two corner reflectors. The sub-meter localization accuracy was achieved using only atmospheric correction information available in the TSX metadata. 相似文献
5.
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
6.
7.
Interpolation-free coregistration and phase-correction of airborne SAR interferograms 总被引：1，自引：0，他引：1
This letter discusses the detection and correction of residual motion errors that appear in airborne synthetic aperture radar (SAR) interferograms due to the lack of precision in the navigation system. As it is shown, the effect of this lack of precision is twofold: azimuth registration errors and phase azimuth undulations. Up to now, the correction of the former was carried out by estimating the registration error and interpolating, while the latter was based on the estimation of the phase azimuth undulations to compensate the phase of the computed interferogram. In this letter, a new correction method is proposed, which avoids the interpolation step and corrects at the same time the azimuth phase undulations. Additionally, the spectral diversity technique, used to estimate registration errors, is critically analyzed. Airborne L-band repeat-pass interferometric data of the German Aerospace Center (DLR) experimental airborne SAR is used to validate the method. 相似文献
8.
In this paper, the registration of decimeter-resolution airborne multi-aspect SAR (MASAR) data of inner city areas by application of the radargrammetric range-Doppler equations is investigated. The geometrical model is adapted to linear flight trajectories and zero-Doppler processed SAR data, whereas the observed trajectory parameters are adjusted using a strict Gauss–Helmert model and known ground control points. The significance of the estimated corrections is examined and the most suitable set of free parameters is determined. Finally, the methodology is applied to real test data of an airborne campaign over the city of Munich, Germany, and the feasability of the proposed radargrammetric registration method is shown. 相似文献
9.
机载SAR影像主动定位的数学模型研究 总被引：1，自引：0，他引：1
本文基于差分GPS(Differential Global Positioning System,DGPS)和惯性导航系统(Inertial Navigation System,INS)数据,在无控制点的情况下,导出了一种进行机载SAR影像主动定位的数学模型。此模型包括DGPS/INS数据进行坐标系转换、天线动态偏心改正、雷达天线相位中心插值和距离-多普勒(Range-Doppler,R-D)模型及解算。根据距离-多普勒(Range-Doppler,R-D)模型和数字高程模型(Digital Elevation Model,DEM)数据,获得机载SAR影像上每点所对应的地理坐标,重采样生成正射影像图。本文通过成都测区1m分辨率的机载SAR影像主动定位试验,验证了此数学模型的正确性,分析了主要系统误差源及系统误差的改正方法。 相似文献
10.
基于有理函数模型的星载SAR影像几何校正 总被引：1，自引：0，他引：1
主要研究了面向星载合成孔径雷达SAR(Synthetic Aperture Radar)影像几何处理的有理函数模型RFM(Rational Function Model)的建模、求解和应用方法。首先采用与地形无关的方式,利用严密的距离-多普勒模型(Range Doppler,RD)构建虚拟控制点格网来进行RFM建模,实现了一种RFM模型参数的快速无偏解算新方法,能够取得相对于RD模型很高的拟合精度,在几何定位功能上实现了对RD模型的有效替代,同时大大提高了计算效率。然后在此基础上利用RFM模型实现了星载SAR影像的快速几何校正,为了提高几何校正结果的绝对定位精度,引入少量地面控制点对RFM模型进行了像方改正处理,以消除SAR影像几何定位的系统误差,并利用ENVISAT ASAR数据的实验结果验证了本文方法的有效性。 相似文献
11.
ABSTRACT In this paper, we propose a method to regenerate Rational Polynomial Coefficients (RPCs) using KOMPSAT-3A imagery and to reduce the geolocation error using minimum ground control points (GCPs). To estimate the new RPCs, the physical sensor model fitted to KOMPSAT-3A imagery was utilized and virtual GCPs over the study area were created. The size of the virtual grid used was 20x20x20. To remove the sensor-related errors in physical sensor model, three different image correction models (image coordinate translation model, shift and drift model, and affine transformation model) were additionally applied. We evaluated our proposed method in two areas within Korea, one in urban (Seoul) and one in rural (Goheung) areas. The results showed that there was a significant improvement after applying the suggested approach in the two areas. The image coordinate translation model is suggested in terms of GCP requirement and expected errors estimated from the error propagation analysis using Gauss–Markov Model (GMM). 相似文献
12.
13.
用多方向飞行的全极化SAR图像可能提取特定三维目标的高度与位置信息,进而实现目标物的几何立体重构。全极化SAR图像数据与单极化SAR相比,可以选择多种极化组合数据,提供对于特定目标几何特征敏感的数据类型,通过多方向飞行SAR图像反演该目标或目标群的高度与位置信息。本文用两幅相向飞行的PI-SAR(日本机载极化与干涉SAR,X波段、1.5m分辨率)图像,提取日本仙台电视塔高度、日本东北大学建筑物群的立体重构。 相似文献
14.
Assessment of long-range kinematic GPS positioning errors by comparison with airborne laser altimetry and satellite altimetry 总被引：3，自引：0，他引：3
Long-range airborne laser altimetry and laser scanning (LIDAR) or airborne gravity surveys in, for example, polar or oceanic
areas require airborne kinematic GPS baselines of many hundreds of kilometers in length. In such instances, with the complications
of ionospheric biases, it can be a real challenge for traditional differential kinematic GPS software to obtain reasonable
solutions. In this paper, we will describe attempts to validate an implementation of the precise point positioning (PPP) technique
on an aircraft without the use of a local GPS reference station. We will compare PPP solutions with other conventional GPS
solutions, as well as with independent data by comparison of airborne laser data with “ground truth” heights. The comparisons
involve two flights: A July 5, 2003, airborne laser flight line across the North Atlantic from Iceland to Scotland, and a
May 24, 2004, flight in an area of the Arctic Ocean north of Greenland, near-coincident in time and space with the ICESat
satellite laser altimeter. Both of these flights were more than 800 km long. Comparisons between different GPS methods and
four different software packages do not suggest a clear preference for any one, with the heights generally showing decimeter-level
agreement. For the comparison with the independent ICESat- and LIDAR-derived “ground truth” of ocean or sea-ice heights, the
statistics of comparison show a typical fit of around 10 cm RMS in the North Atlantic, and 30 cm in the sea-ice region north
of Greenland. Part of the latter 30 cm error is likely due to errors in the airborne LIDAR measurement and calibration, as
well as errors in the “ground truth” ocean surfaces due to drifting sea-ice. Nevertheless, the potential of the PPP method
for generating 10 cm level kinematic height positioning over long baselines is illustrated. 相似文献
15.
The goal of the OSIRIS-REx mission is to return a sample of asteroid material from near-Earth asteroid (101955) Bennu. The role of the navigation and flight dynamics team is critical for the spacecraft to execute a precisely planned sampling maneuver over a specifically selected landing site. In particular, the orientation of Bennu needs to be recovered with good accuracy during orbital operations to contribute as small an error as possible to the landing error budget. Although Bennu is well characterized from Earth-based radar observations, its orientation dynamics are not sufficiently known to exclude the presence of a small wobble. To better understand this contingency and evaluate how well the orientation can be recovered in the presence of a large 1\(^{\circ }\) wobble, we conduct a comprehensive simulation with the NASA GSFC GEODYN orbit determination and geodetic parameter estimation software. We describe the dynamic orientation modeling implemented in GEODYN in support of OSIRIS-REx operations and show how both altimetry and imagery data can be used as either undifferenced (landmark, direct altimetry) or differenced (image crossover, altimetry crossover) measurements. We find that these two different types of data contribute differently to the recovery of instrument pointing or planetary orientation. When upweighted, the absolute measurements help reduce the geolocation errors, despite poorer astrometric (inertial) performance. We find that with no wobble present, all the geolocation requirements are met. While the presence of a large wobble is detrimental, the recovery is still reliable thanks to the combined use of altimetry and imagery data. 相似文献
16.
利用航摄像片存在的相对几何位置关系,将机载IMU视准轴误差引入立体像对相对定向模型中,提出了一种基于相对定向的机载IMU视准轴误差求解新方法。详细推导了基于单个立体模型和连续立体模型求解IMU视准轴误差的数学模型,并用三组带有IMU设备获取的实际航空影像数据进行了试验验证。结果表明,所推导的机载IMU视准轴误差求解方法是正确、可行的,利用三张以上相邻像片构成的连续立体模型即可求解出IMU的视准轴误差,避免了野外布设检校场和其他地面控制条件带来的诸多问题,有利于带机载IMU的航空遥感快速对地目标定位。 相似文献
17.
基于参考DEM的机载InSAR定标方法 总被引：1，自引：0，他引：1
研究无人工靶标的干涉定标方法对促进机载InSAR技术在山区等复杂地形的测绘、制图等定量应用有重要的实用价值。本文提出一种新的基于参考DEM的干涉定标方法,在InSAR定标中用已知高程精度的参考DEM与待定标的InSAR系统生成的DEM进行比较,利用参考DEM模拟SAR图像,获得大量定标所需的控制点坐标来建立敏感度矩阵,并对敏感度方程的解算进行了改进,同时将干涉处理与定标过程相结合,改进了干涉处理过程,最后得到定标后的干涉参数并生成DEM,利用机载数据进行了实验验证,并分析了无人工靶标干涉定标实验结果的误差。 相似文献
18.
探讨了可见光立体像对遥感数据在森林平均树高估算研究方向的可行性,为解决大区域快速提取森林平均树高参数的科学问题提供技术支撑。利用GeoEye-1卫星立体像对中提供的有理多项式系数(RPC)参数和数字表面模型(DSM)与数字高程模型(DEM)的理论原理,建立了基于DSM和DEM空间相差模型建立林分冠层高度估算方法流程。结果表明:基于湖南攸县黄丰桥国有林场GeoEye-1立体像对影像数据,按照估算流程,最终得到试验区小班尺度的样地平均树高遥感提取结果。结合样地地面实测控制点和地面小班数据调查数据,该方法提取的研究区平均树高总体误差率在83.1%,其中最大误差为3.773 m,最小误差为0.025 m。因此,本研究是一种可以快速获得研究区大范围森林平均树高参数的创新、可行的方法。 相似文献
19.
配准作为干涉处理过程中的重要一步,其精度直接影响后续的处理。机载重复轨道干涉数据,由于飞行的姿态不一致,导致影像间产生较大的相对变形,常规的方法无法对整幅影像进行配准。本文结合SIFT匹配算法的稳健性和解析搜索配准算法高精度的优点,利用飞行轨道间的关系和统计分析剔除错误的匹配,提出了一种针对机载重复轨道干涉数据的配准方法,有效解决了机载重复轨道干涉数据的配准问题。首先利用SIFT匹配算法提取一定数量的匹配点,然后利用飞行轨道之间的关系和对匹配点偏移量的统计分析,剔除误匹配的点,完成粗配准,最后使用解析搜索算法完成精配准。本文利用国产CASMSAR系统获取的机载P波段重复轨道干涉数据进行实验,取得了良好的效果。 相似文献
20.
风云3号B星(FY-3B)上的微波成像仪(MWRI)通过10.65 GHz,18.7 GHz,23.8GHz,36.5 GHz和189.0 GHz5个频率的双极化通道对地球表面进行监测。自卫星发射至今,MWRI资料的地理定位误差还未进行深入研究。为了提高FY-3B MWRI L1级数据地理定位精度,基于海、陆响应的升、降轨亮温差理论NDM(Node Differential Method),通过卫星位置和速度矢量建立卫星姿态模型、采用非线性最优化方法估计卫星姿态偏差,进而对MWRI 89 GHz通道的地理定位误差进行分析与订正。结果表明,2015年1—9月份俯仰、滚动和偏航角度的平均偏差分别为-0.220°,0.068°和0.062°,对应沿轨误差大约3—4 km,跨轨误差小于1 km。定位误差订正后,地中海、澳大利亚区域海岸线附近的升降轨亮温差明显减小;观测亮温在红海和南美洲东南部区域的分布和海岸线更加吻合,定位精度得到明显提高。 相似文献