The invention discloses a spatial distributed
observation method based on irregular region geometric feature sampling, and belongs to the technical field of
aerospace. The implementation method comprises the following steps: establishing a coordinate
system for describing the motion of the
spacecraft; establishing a
spacecraft dynamic model under the coordinate
system; six initial
orbit elements of a
satellite can be obtained based on existing low-
orbit constellation orbit data, the spatial position is calculated through the orbit elements, and then position components are converted into
latitude and
longitude coordinates, namely sub-
satellite point coordinates; defining vertex coordinates of the polygon, and constructing a
planar polygon by connecting the vertex coordinates end to end; discretizing the internal region of the closed polygon; on the basis of the
kinetic model, on the basis of the coordinates of the sub-
satellite point and the center coordinates of the discrete sampling circle, calculating the characteristic distance from the sampling point in the observation area to the sub-satellite point, and on the basis of the size relationship between the characteristic distance and the
radius of the observation view field, judging whether the irregular area can be successfully observed in a preset time constraint interval; therefore, spatial distributed observation is realized.