Spaceflight optical remote sensing imaging simulation method based on space-time unified feature
An optical remote sensor and simulation method technology, applied in the field of aerospace optical remote sensing, can solve the problems that have not yet been discovered, do not involve imaging link signal, noise and MTF simulation, cannot realize on-orbit image simulation, etc., so as to improve imaging quality and ensure The effect of accuracy
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[0031] like figure 1 As shown, it is the specific implementation way of the method of the present invention.
[0032] (1) Determination of satellite orbit parameters:
[0033] First, according to user needs, set six numbers of satellite orbits: true perigee angle, argument of perigee, orbital inclination, ascending node right ascension, eccentricity and orbital semi-major axis to determine the orbit of the satellite after it goes to the sky.
[0034] Before calculating the satellite orbit parameters, we must first introduce the two coordinate systems used: the geocentric orbit coordinate system and the equatorial inertial coordinate system.
[0035] The geocentric orbital coordinate system is: the origin O is at the center of the earth, x 0 The axis points from the center of the earth to the spacecraft, that is, along the distance vector r, y from the center of the earth 0 The axis is in the orbital plane, perpendicular to the vector r, pointing forward, z 0 The axes are p...
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