Global communication constellation designing method for realizing on-demand coverage of key areas
A key area and design method technology, applied in the field of satellite communication, can solve problems such as complex system control, fast movement of low-orbit satellites, and high technical risks, and achieve the effects of low complexity, reduced number of satellites, and system economy
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[0029] The present invention proposes a global communication constellation design method for on-demand coverage of key areas, figure 1 A flow chart of the steps of the method of the present invention, the constellation designed by the method can provide communication coverage services at high elevation angles for specific regions in the southern / northern hemispheres.
[0030] Before introducing the realization method of the present invention, at first define under the geocentric inertial system the orbit 6 numbers that describe satellite state, refer to figure 2 , the number of orbital elements and their functions are as follows:
[0031] (1) Orbit shape parameters a and e: a is the semi-major axis of the orbit, and e is the eccentricity of the orbit.
[0032] (2) Orbital plane parameters i and Ω: i is the orbital inclination, and Ω is the right ascension of the ascending node, that is, the angle turned from the X axis to the ascending node in the X-Y plane.
[0033] (3) Ar...
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