Abstract
This paper proposes a multi-baseline method to estimate absolute coordinates of point clouds and the camera attitude parameter utilizing feature points in successive images. Conventionally, 3D map generation methodologies have been based on images acquired by aerial or land vehicles. Pixels corresponding to known landmarks are manually identified at first. Next, the coordinates are directly geo-referenced and automatically allocated to pixels with high-quality Global Positioning System (GPS) and Inertial Navigation System (INS). However, it is difficult to obtain accurate coordinates by the conventional methodology with low-cost GPS and INS. With camera positions and attitude parameters, image-based point clouds can be compensated accurately. A simulation was carried out to evaluate the performance of the proposed method.
Highlights
This paper proposes a method to estimate threedimensional (3-D) coordinates of point clouds and attitude parameters simultaneously by two-dimensional (2-D) matched feature points in two successive images
The proposed method to estimate absolute coordinates of point clouds and to compensate error of attitude parameters is briefly explained by pictures
Error of attitude parameters from Global Positioning System (GPS)/Inertial Navigation System (INS) Kalman outputs can be compensated by 2-D feature points extracted from the images
Summary
This paper proposes a method to estimate threedimensional (3-D) coordinates of point clouds and attitude parameters simultaneously by two-dimensional (2-D) matched feature points in two successive images. To extract feature points and to match them in the two successive images, Speeded-Up Robust Feature (SURF) algorithm is utilized [4]. A loosely-coupled Kalman filter is applied to estimate absolute coordinates of the camera and its attitude parameters. With these parameters and error of them, image-based point clouds are compensated and converted to absolute coordinates of them. The proposed method to estimate absolute coordinates of point clouds and to compensate error of attitude parameters is briefly explained by pictures.
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