Imaging Simulation Method for Aerospace Optical Remote Sensor Based on the Unified Characteristics of Time and Space
A technology of optical remote sensor and simulation method, which is applied in the field of aerospace optical remote sensing, can solve problems that have not been discovered, have not involved imaging link signal, noise and MTF simulation, and cannot realize on-orbit image simulation, so as to improve imaging quality and ensure The effect of accuracy
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[0031] Such as figure 1 Shown is the specific implementation approach of the method of the present invention.
[0032] (1) Determination of satellite orbit parameters:
[0033] First, according to the user's needs, set the six numbers of the satellite orbit: true anomaly, argument of perigee, orbital inclination, right ascension of ascending node, eccentricity, and semi-major axis of the orbit to determine the orbit of the satellite after it goes into the sky.
[0034] Before calculating the satellite orbit parameters, we must first introduce the two coordinate systems used: the geocentric orbital 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 center of gravity vector r, y 0 Axis in orbital plane, perpendicular to vector r, pointing forward, z 0 The axis is perpendicular to...
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