研究目的
The goal of this study is to develop and present a new method that computes the trajectory of the laser instrument using the point cloud. We evaluate the resulting trajectories using ALS data from five acquisitions across different biomes in the United States Pacific Northwest region and compare the computed trajectory to the trajectory recorded during the data acquisition.
研究成果
The method developed in this study is robust and produces trajectories that compare well to those recorded as part of the original data collection effort. While error varies by acquisition, the error in the computed aircraft position seldom exceeded a few meters. The resulting trajectories are sufficient for all applications requiring them. However, the success of the method relies on data where pulses have at least two returns, which may not be available in areas with little or no vegetation.
研究不足
The method relies on data where pulses have at least two returns, which may not be available in areas with little or no vegetation. The accuracy of the method may be affected by the spatial distribution of multiple returns and the presence of outliers in the data.
1:Experimental Design and Method Selection:
The study used ALS data from five acquisitions in the US Pacific Northwest region states of Oregon and Washington. The method involves recovering aircraft positions using only the point cloud by calculating the intersection or closest point of approach of multiple-return pulses. A cubic spline is fit to the intersection points to provide a continuous trajectory.
2:Sample Selection and Data Sources:
ALS data from five acquisitions in the US Pacific Northwest region states of Oregon and Washington were used. The data included the smoothed best estimate of trajectory (SBET) provided for the acquisitions.
3:List of Experimental Equipment and Materials:
Airborne laser scanning (ALS) data, point cloud data, and trajectory data were used.
4:Experimental Procedures and Operational Workflow:
The method involves calculating the intersection or closest point of approach of multiple-return pulses and fitting a cubic spline to these points to estimate the aircraft trajectory.
5:Data Analysis Methods:
The derived aircraft positions were validated using the SBET provided for the acquisitions. The error in the computed aircraft position was analyzed.
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