Orbit correction requirements for a natural resources satellite

Details Orbit correction requirements for a natural resources satellite Orbit correction requirements for a natural resources satellite

Aug 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987cobe.cong....7c&link_type=abstract

Presented at the 9th Brazilian Congress of Mechanical Engineering, COBEM/87, 7-11 Dec. 1987, Florianopolis, Santa Catarina

Physics

Correction, Orbit Calculation, Orbit Decay, Orbital Mechanics, Satellite Perturbation, Aerodynamic Drag, Artificial Satellites, Earth Observations (From Space), Flight Mechanics, Gravitational Effects

Scientific paper

The decay of the semimajor axis and the inclination of the orbit of an artificial Earth observation satellite is analyzed, considering the atmospheric drag perturbations in the former case and the lunar-solar gravitational attraction perturbations in the latter case. Finally, the orbit correction requirements, necessary for maintaining the satellite in the desired orbit, are defined.

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