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The DG Performance Verifications of UAV Borne MMS Payload with Two Tactical Grade Low Cost MEMS IMUs Using New Calibration Method

机译:使用新校准方法,UAV的DG性能验证与两个战术级低成本MEMS IMU有两个战术级低成本MEMUS

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Rapid spatial information collection has become an emerging trend for remote sensing and mapping applications. To facilitate applications such as environment detection and disaster monitoring, the development of rapid low cost systems for collecting near-real-time spatial information is very critical. The technology of Unmanned Aerial Vehicle (UAV) mobile mapping system (MMS) can satisfy these demands. It usually loads an Inertial Navigation System (INS) and Global Positioning System (GPS) for integrated positioning and orientation. Moreover, the mapping system is also loaded on board to implement of Direct Georeferencing (DG) capability. The DG capability can rapidly provide the coordinate of interesting points without any ground control points. These coordinates can be quickly converted to measurable spatial information for numerous applications demanding for near real time georeferenced images. This study develops a long endurance DG based fixed-wing UAV photogrammetric platform where a low cost tactical grade integrated Positioning and Orientation System (POS) is developed. In addition, a novel kinematic calibration method including lever arms, boresight angles and camera shutter delay is proposed. A commercial Micro Electro Mechanical Systems (MEMS) tactical grade IMU is also applied for comparison. Two flight tests with two tactical grade low cost MEMS IMUs are performed to verify the positioning accuracy in DG mode without using Ground Control Points (GCPs) using different calibration method. This study develops a new two-step-kinematic calibration method and compares with traditional two-step calibration. Furthermore, the performance of DG is also analyzed based on the two methods with the different flights and two DG modules. The results presented in this study indicate the accuracy of DG can be significantly improved by lower flight and hardware with superior specifications. The new two-step-kinematic method improves the accuracy of DG about 1-10%. The preliminary results show that horizontal DG positioning accuracies in two-dimension (2D) are around 8 m at a flight height of 600 m with the newly designed tactical grade integrated Positioning and Orientation System (POS). The positioning accuracy in three-dimension (3D) is less than 12 m. Such accuracy is good for near real-time disaster relief. The DG ready function of the proposed platform guarantees mapping and positioning capability even in GCP free environments, which is very important for rapid urgent response for disaster relief. Generally speaking, the data processing time for the DG module, including POS solution generalization, interpolation, Exterior Orientation Parameters (EOP) generation, and feature point measurements, is less than one hour.
机译:快速空间信息收集已成为遥感和映射应用的新兴趋势。为了促进环境检测和灾害监测等应用,用于收集近实时空间信息的快速低成本系统的开发非常关键。无人驾驶飞行器(UAV)移动映射系统(MMS)的技术可以满足这些需求。它通常加载惯性导航系统(INS)和全球定位系统(GPS),用于集成定位和方向。此外,映射系统还装载到电路板上,以实现直接地地理率(DG)能力。 DG能力可以快速提供有趣点的坐标,而无需任何地面控制点。这些坐标可以快速转换为可测量的空间信息,以获得许多要求近乎实时地理参考图像的众多应用。本研究开发了一种基于长的基于DG的固定翼UAV摄影测量平台,其中开发了低成本的战术级集成定位和方向系统(POS)。另外,提出了一种包括杠杆臂,触觉角度和相机快门延迟的新型运动校准方法。商业微电机械系统(MEMS)战术等级IMU也用于比较。进行两次飞行试验,进行两个战术级低成本MEMS IMU,以验证DG模式下的定位精度,而无需使用不同的校准方法的地面控制点(GCP)。本研究开发了一种新的两步运动校准方法,并与传统的两步校准进行比较。此外,还基于具有不同飞行和两个DG模块的两种方法分析DG的性能。本研究中提出的结果表明DG的准确性通过较低的飞行和硬件可以显着提高,具有优异的规格。新的两步运动方法提高了约1-10%的准确性。初步结果表明,在三维(2D)中的水平DG定位精度为600米的飞行高度约为8米,具有新设计的战术级集成定位和方向系统(POS)。三维(3D)中的定位精度小于12米。这种准确性适用于近实时救灾。即使在GCP自由环境中,所提出的平台的DG Ready功能也可以保证映射和定位功能,这对于救灾快速响应的快速响应非常重要。一般而言,DG模块的数据处理时间,包括POS解决方案泛化,插值,外向方向参数(EOP)生成和特征点测量,小于一小时。

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