A Method of Target Star Selection for Manned Asteroid Exploration
A technology of asteroids and target stars, applied in the field of aerospace, can solve problems such as many qualitative analysis, low scientific level, complicated screening process, etc.
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[0035] The present invention will be further described below in conjunction with accompanying drawing.
[0036] Depend on image 3 As can be seen, the present invention provides a method for selecting a target star for manned asteroid detection, which comprises the following steps:
[0037] Step 1: Determine the constraints for the primary selection of the target star
[0038] The constraints for the primary selection of the target star are composed of asteroid orbital parameters, the asteroid's absolute magnitude, and the asteroid's spin period, and each part is in a parallel relationship.
[0039] The asteroid orbit parameters include the semi-major axis a, eccentricity e, and orbit inclination i of the asteroid orbit. It is determined by the carrying capacity of the launch vehicle and is the primary factor considered in the primary selection of the target star. In this example a min max , e1 ,e 2}, imin ,a max ,e 1 ,e 2 The calculation formula is
[0040]
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