The invention relates to a
space debris angle measurement
data simulation method. The method comprises the steps of dynamically receiving and loading observation plan data of observation equipment by loading polar shift data, dynamically loaded observation equipment
information data and dynamically inputting
system errors and random errors of the equipment, according to information such as the spatial debris position and speed in a J2000
inertial coordinate system received in real time, converting into a
space debris station center position under the J2000 inertial
system to obtain a horizontal
right ascension and a horizontal
declination of the
space debris under the J2000 inertial
system and a
right ascension and a
declination of the space debris under a
station center
equator coordinate system, further converting into an
azimuth and a
pitch under a
horizon coordinate, and adding a
system error, a
random error and a wild value to generate space debris angle measurement
simulation data. According to the method, by loading the observation plan data, the space debris can be observed in a planned manner, the consistency of the
simulation environment and the real observation environment is ensured in the
simulation process, and the simulation efficiency of the angle measurement data is improved.