The application relates to a kind of
asteroid surface escape velocity calculation method considering rotation and
terrain influence, comprising: obtaining the three-dimensional shape model of target
asteroid and carrying out discrete, reading the vertex set and
triangular facet set of polyhedron, carrying out gravity field modeling, establishing standard polyhedral gravity model;Define the logarithmic kernel function of each edge of each
triangular facet, to determine the
gravitational potential of target
asteroid on any
field point;Establish star-fixed coordinate
system in standard polyhedral gravity model, determine the rotation speed of any point on the surface of target asteroid, thereby define the
effective potential upper bound and the inertial
system speed of the release instant of the particle on the surface of target asteroid;Based on the minimum escape condition that the
kinetic energy of the particle on the surface of target asteroid is equal to the corresponding
effective potential upper bound, determine the minimum normal escape velocity of the particle. Compared with the prior art, the application can quickly obtain accurate minimum escape velocity and corresponding escape direction at any
surface point.