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Differential orbit correction and station locator program doc - ii
The analysis and programming associated with performing a differential correction to orbital elements and/or station positions from weighted observations of range, range rate, azimuth-elevation and/or right ascension-declination on close earth satellites are described. The ephemeris computation considers perturbations due to the earth's gravitational potential as described by a spherical harmonic representation through n = m = 5, the lunar gravitational potential, air drag and radiation pressure. All observations may be simulated in punched card form for the purposes of conducting geometric studies. (Author).
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- http://experiment.worldcat.org/entity/work/data/137065749#Topic/programming_languages
- http://experiment.worldcat.org/entity/work/data/137065749#Topic/artificial_satellites
- http://experiment.worldcat.org/entity/work/data/137065749#Topic/flight_paths
- http://experiment.worldcat.org/entity/work/data/137065749#Topic/differential_equations
- http://experiment.worldcat.org/entity/work/data/137065749#Topic/computer_programming
- http://experiment.worldcat.org/entity/work/data/137065749#Topic/orbits
http://schema.org/description
- "The analysis and programming associated with performing a differential correction to orbital elements and/or station positions from weighted observations of range, range rate, azimuth-elevation and/or right ascension-declination on close earth satellites are described. The ephemeris computation considers perturbations due to the earth's gravitational potential as described by a spherical harmonic representation through n = m = 5, the lunar gravitational potential, air drag and radiation pressure. All observations may be simulated in punched card form for the purposes of conducting geometric studies. (Author)."@en
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- "Differential orbit correction and station locator program doc - ii"@en