The invention relates to the technical field of
aerospace, in particular to a
space debris environment quantification method based on risk entropy, and the method comprises the steps: S1, discretizing an evaluation
time range into a plurality of time periods, and recording the duration of each time period as
delta t; any time period tj can be expressed as tj belongs to [(j-1) *
delta t, j *
delta t]; j < = N, where N represents the total number of time periods;
simulation is carried out, and it is assumed that N + 1 possibilities exist in the in-
orbit collision disintegration condition of the
space object objk; specifically, if N time periods exist, there is N possibilities for the
space object to collide and disintegrate; if the
space object is still not disassembled at the end of
simulation, judging that N + 1 possibilities exist in collision and disassembly of the space object; s2, calculating a
collision probability in a time period; and S3, calculating a risk entropy according to the
collision probability, and judging the influence of the space object on the
space debris environment according to the risk entropy. The
space debris environment quantification method based on the risk entropy can be used for quantification of uncertainty of the space debris environment.