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Volume 40 Issue 3
Mar.  2014
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Journal of Beijing University of Aeronautics and Astronautics  > 2014  >  40(3): 377-382.
Su Qinghua, Zhao Yan, Yang Kui, et al. Hover-stage lunar lander autonomous relatively navigation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 377-382. doi: 10.13700/j.bh.1001-5965.2013.0244(in Chinese)
Citation: Su Qinghua, Zhao Yan, Yang Kui, et al. Hover-stage lunar lander autonomous relatively navigation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(3): 377-382. doi: 10.13700/j.bh.1001-5965.2013.0244(in Chinese)
shu

Hover-stage lunar lander autonomous relatively navigation

doi: 10.13700/j.bh.1001-5965.2013.0244

  • School of Instrumentation Science and Opto-electronics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 06 May 2013
  • Publish Date: 20 Mar 2014
    Abstract
  • The lunar lander landing phase navigation information analysis is a key to achieve the safety soft landing on lunar surface. According to requirements for the hover-stage navigation, the lunar lander carrying equipment and its access to the characteristics of the lunar surface, laser rangefinder and optical navigation camera optical were used in autonomous relative navigation. A coordinate system relative navigation was created. According to the relationship between the various coordinate systems, the transformation matrix and navigation information was determined, the position and attitude of the lander relative lunar landing point was estimated. Finally, the method was verified by simulation experiments. Results show that this method can calculate relative position, posture fast and accurately. The method is valuable for further steps of moon exploration projects, and can be used as soft-landing close relative navigation for Mars and other asteroids exploration.

     

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