Optimizing initial inclinations and RAANs of a satellite...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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C701S226000

Reexamination Certificate

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07664578

ABSTRACT:
A method for minimizing the amount of propellant required to be carried onboard the satellites of an Earth orbiting satellite constellation to maintain the minimum angle of elevation between a selected geographical area of the Earth and at least one satellite of the constellation during the life of the constellation includes establishing an optimal initial inclination and RAAN of each satellite of the constellation. The method enables the satellites of the constellation to carry additional hardware and other payload mass, or alternatively, the design life of the constellation to be increased.

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Kechichian, “Orbit Plane Control Strategies for Inclined Geosynchronous Satellite Constellation”, Journal of Spacecraft and Rockets, vol. 35, No. 1, Jan 1998 (pp. 9).

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