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Ephemeris / Astronomical unit / Kepler orbit / Perturbation / Numerical integration / Orbit / Axial tilt / Tidal acceleration / Fundamental ephemeris / Celestial mechanics / Astrology / Astronomy


Document Date: 2004-04-06 10:49:50

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City

Napoli / /

Company

Jet Propulsion Laboratory / GM / /

Country

Netherlands / /

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Facility

Jet Propulsion Laboratory / /

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recursive algorithm / numerical algorithm / integration algorithm / unnecessary computing effort / dx4 processor / individual hardware / conventional extrapolation algorithm / /

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Venus / Mercury / Mars / /

Organization

US Federal Reserve / /

Person

Federico II / /

Position

Major / /

Product

DE200 / /

Technology

numerical algorithm / conventional extrapolation algorithm / recursive algorithm / integration algorithm / 486 dx4 processor / /

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