The invention discloses a classical
orbit three-dimensional
spatial relationship construction method based on an OSG three-dimensional engine. Spatial relationships are directly established based on six elements of an orbital
system, and geometrical angle changing processes of the
right ascension of an ascending node, the
orbit inclination, the perigee argument and the true anomaly can be dynamically displayed. An orbital element parameter representation process is based on the space geometry relationships, and
satellite visual angle tracking and position calculation are not subjected to secondary coordinate transformation. The
orbital elements can be visually displayed, and an orbital
system (VVLH)
visual angle positioning problem under a traditional model is solved by the introduction of two
layers of new coordinate systems. Four attitude input interfaces of matrixes,
Euler angles, Euler axial angles and the
quaternion of a relative orbital
system are provided by a
spacecraft, and the
spacecraft body axis and the
orbit axis are displayed and customized through the
spacecraft, the analysis of the
correctness of the in-orbit attitude of the spacecraft is facilitated, and problems that the
orbital elements cannot be visually displayed, the
orbital elements need the secondary transformation, the attitude adjustment and
visual angle adjustment of the orbital system require additional data, and the position and orientation of the spacecraft cannot be accurately displayed are solved.