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Pose Tracking of a Noncooperative Spacecraft During Docking Maneuvers Using a Time-of-Flight Sensor

机译:使用飞行时间传感器对接的非合作航天器的姿态跟踪

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This paper presents a pose estimation procedure for tracking attitude and position of a noncooperative tumbling spacecraft during rendezvous and docking maneuvers. The key aspect of the method is that the current state of the target spacecraft is estimated in real-time using a low-resolution depth-image of the scene and a known model of the vehicle. The proposed procedure exploits the iterative closest point algorithm implemented in closed-loop fashion. In order to guarantee stability of the solution, the current pose of the target is predicted onboard by propagating the last estimated state using a dedicated dynamics model of the maneuver. The tracking procedure is initialized with a fast template matching algorithm that determines attitude and position of the target without prior information on its state. The capabilities of the proposed procedure are demonstrated using a full degrees-of-freedom hardware simulator. In these experiments, the Microsoft Kinect v2 sensor is employed for real-time acquisition of the target spacecraft depth image. The results demonstrate the effectiveness of the proposed procedure during docking maneuvers to a noncooperative tumbling target However, prediction of the current target pose is crucial for algorithm robustness.
机译:本文提出了一个姿势估计程序,用于在交会和对接演习中跟踪非合作翻滚航天器的姿态和位置。该方法的关键方面是使用场景的低分辨率深度图像和飞行器的已知模型实时估算目标航天器的当前状态。所提出的过程利用了以闭环方式实现的迭代最近点算法。为了保证解决方案的稳定性,使用专用的动力学模型通过传播最后的估计状态,在船上预测目标的当前姿态。跟踪过程使用快速模板匹配算法初始化,该算法确定目标的姿态和位置,而无需事先提供有关其状态的信息。使用完整的自由度硬件模拟器演示了所建议过程的功能。在这些实验中,Microsoft Kinect v2传感器用于实时获取目标航天器深度图像。结果证明了拟议程序在对接非合作翻滚目标过程中的有效性。但是,当前目标姿态的预测对于算法的鲁棒性至关重要。

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