Visual autonomous navigation method of satellite relative to minor planet
A navigation method and visual autonomy technology, which can be used in integrated navigators and other directions, and can solve problems such as lack of asteroid information
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[0097] The technical solution of the present invention will be further introduced below in combination with specific implementation methods and accompanying drawings.
[0098] This specific embodiment discloses a satellite-relative asteroid visual autonomous navigation method, such as figure 1 and figure 2 As shown, it is aimed at the asteroid deep space exploration stage, and the satellite uses the star sensor to independently and continuously observe the asteroid for autonomous navigation, which is a very suitable autonomous navigation method for deep space exploration satellites. Specifically include the following steps:
[0099] S1: Taking the target asteroid as the tracking observation object, according to the asteroid ephemeris, design the theoretical flight orbit parameters of the satellite; among them, the theoretical flight orbit parameters of the satellite include orbital semi-major axis a, orbital eccentricity e, orbital inclination i, ascending node redness Long...
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