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Design and test of a simulation system for autonomous optic-navigated planetary landing

机译:自主光学导航行星着陆仿真系统的设计与测试

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In this paper, a simulation system based on commercial projector is proposed to test the optical navigation algorithms for autonomous planetary landing in laboratorial scenarios. The design work of optics, mechanics and synchronization control are carried out. Furthermore, the whole simulation system is set up and tested. Through the calibration of the system, two main problems, synchronization between the projector and CCD and pixel-level shifting caused by the low repeatability of DMD used in the projector, are settled. The experimental result shows that the RMS errors of pitch, yaw and roll angles are 0.78'. 0.48'. and 2.95' compared with the theoretical calculation, which can fulfill the requirement of experimental simulation for planetary landing in laboratory.
机译:本文提出了一种基于商用投影仪的仿真系统,以测试实验室场景中自主行星着陆的光学导航算法。进行了光学,机械和同步控制的设计工作。此外,整个仿真系统已建立并经过测试。通过系统的校准,解决了两个主要问题,即投影仪和CCD之间的同步以及投影仪中使用的DMD的低重复性导致的像素级偏移。实验结果表明,俯仰角,横摆角和横摆角的均方根误差为0.78'。 0.48'。与理论计算值相比为2.95',可以满足实验室对行星着陆实验仿真的要求。

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