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Autonomous optical navigation for landing on asteroids

机译:自主光学导航,可登陆小行星

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Purpose - In order to succeed in landing asteroids, good accuracy autonomous navigation is absolutely necessary. Aims to describe a new autonomous navigation algorithm. Design/methodology/approach - First, gray images of asteroid surface are acquired by optical navigation camera, and nature feature points are detected and tracked autonomously. Second, the directional vector from spacecraft to the center of each feature point can be computed from the image coordinates in camera focal plane. Then, LIDAR/LRF is directed to three feature points and the distances from spacecraft to feature points are obtained. Last, the relative position vector from spacecraft to the target asteroid is reconstructed base on measurement outputs of navigation cameras and laser light radar (laser range finder). Findings - Suppose the initial conditions presented in this paper, the autonomous optical navigation position error and velocity error are less than 1 m and 0.1 m/s, respectively; this navigation accuracy can satisfy the requirement of soft landing on asteroids. Originality/value - Based on feature detection and tracking, an autonomous optical navigation scheme is brought out and the validity is confirmed by computer simulation.
机译:目的-为了成功地使小行星着陆,绝对必要的是要有高精度的自主导航。旨在描述一种新的自主导航算法。设计/方法/方法-首先,通过光学导航摄像机获取小行星表面的灰度图像,并自动检测和跟踪自然特征点。其次,可以根据相机焦平面中的图像坐标来计算从航天器到每个特征点中心的方向向量。然后,将LIDAR / LRF指向三个特征点,并获得从航天器到特征点的距离。最后,根据导航摄像机和激光雷达(激光测距仪)的测量输出,重建从航天器到目标小行星的相对位置矢量。发现-假设本文提出的初始条件,自主光学导航位置误差和速度误差分别小于1 m和0.1 m / s;这种导航精度可以满足小行星软着陆的要求。原创性/价值-基于特征检测和跟踪,提出了一种自主的光学导航方案,并通过计算机仿真确认了有效性。

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