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首页> 外文期刊>Journal of optical technology >Star sensor for independent navigation in deep space
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Star sensor for independent navigation in deep space

机译:星型传感器可在深空进行独立导航

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摘要

Astronomical methods of navigation in interplanetary flight, using the directions to the planets and the ephemeris radius vectors of the planets have been used since the late 1960s. These methods have continued to evolve in connection with the performance of experiments in deep space, such as Grand Tour, Venus, Phobos, Ulysses, Galileo, Cassini, and a number of others. Existing star sensors solve navigational problems by processing on-board observations at the command station of the flight. In developing the idea proposed earlier of a star sensor for navigation in the independent regime, a version of the fundamental optical layout is considered, along with original data for developing the technical specification on the production of this device. (c) 2007 optical Society of America.
机译:自1960年代后期以来,就一直使用星际飞行中的天文导航方法,即使用指向行星的方向和行星的星历半径矢量。这些方法随着深空实验的进行而不断发展,例如Grand Tour,Venus,Phobos,Ulysses,Galileo,Cassini等。现有的恒星传感器通过处理飞行指挥站的机载观测值来解决导航问题。在开发较早提出的在独立状态下导航的星形传感器的想法时,考虑了基本光学布局的一种版本,以及用于开发该设备生产技术规范的原始数据。 (c)2007年美国光学学会。

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