Jet Propulsion Laboratory Developmental Ephemeris

The Jet Propulsion Laboratory Developmental Ephemeris or JPL DE is actually a series of computer-based programs for the prediction of high precision coordinates for the Sun, Moon and planets. One of the principal puroses of the JPL DE's is to support both robotic and manned spacecraft missions from the 1960s through the present.

In the 1970s and early 1980s, much work was done in the astronomical community to update the astronomical almanacs from the theoretical work of the 1890s to modern, relativistic theory. From 1975 through 1982, six ephemerides were produced at JPL using the modern techniques of least-squares adjustment of numerically-integrated output to high precision data. Among the most significant of them were the DE102 and DE200.

DE102 was the first numerically integrated so-called Long Ephemeris, covering much of history for which useful astronomical observations were available: 1141 BC to AD 3001. DE200, a version of DE118 rotated to the J2000.0 reference frame, was adopted as the fundamental ephemeris for the new almanacs starting in 1984. The JPL ephemerides have remained the basis of the Astronomical Almanac to the present; the current Almanac is derived from DE405. Each such ephemeris was produced by numerical integration of the equations of motion, starting from a set of initial conditions.

Due to the precision of modern observational data, the analytical method of general perturbations could no longer be applied to a high enough accuracy to adequately reproduce the observations. The method of special perturbations was applied, using numerical integration to solve the n-body problem, in effect putting the entire Solar System into motion in the computer's memory, accounting for all relevant physical laws. The initial conditions were both constants such as planetary masses, from outside sources, and parameters such as initial positions and velocities, adjusted to produce output which was a "best fit" to a large set of observations. A least-squares technique was used to perform the fitting.

The physics modeled include the mutual Newtonian gravitational accelerations and their relativistic corrections, the accelerations caused by the tidal distortion of the Earth, the accelerations caused by the figure of the Earth and Moon, and a model of the lunar librations.

The observational data in the fits has been an evolving set, including: ranges (distances) to planets measured by radio signals from spacecraft, direct radar-ranging of planets, two-dimensional position fixes (on the plane of the sky) by VLBI of spacecraft, transit and CCD telescopic observations of planets and small bodies, and laser-ranging of retroreflectors on the Moon, among others.

The table below lists some of the most important JPL DEs along with a brief description.

JPL Developmental Ephemeris
JPL DE Description
DE102Created September 1981; includes nutations but not librations.
Referred to the dynamical equator and equinox of 1950.
First Long Ephemeris spanning -1410 Apr 16 to 3002 Dec 22 (JED 1206160.5 to JED 2817872.5).
DE200Created September 1981; includes nutations but not librations.
Referred to the dynamical equator and equinox of 2000.
Covers 1599 Dec 09 to 2169 Mar 31 (JED 2305424.5 to JED 2513360.5).
This ephemeris was used for the Astronomical Almanac from 1984 to 2003.
DE202Created October 1987; includes nutations and librations.
Referred to the dynamical equator and equinox of 2000.
Covers 1899 Dec 04 to 2050 Jan 02) (JED 2414992.5 to JED 2469808.5)
DE403Created May 1993; includes nutations and librations.
Referred to the International Celestial Reference Frame.
Covers 1599 Apr 29 to 2199 Jun 22 (JED 2305200.5 to JED 2524400.5).
Fit to planetary and lunar laser ranging data.
DE405Created May 1997; includes both nutations and librations.
Referred to the International Celestial Reference Frame.
Covers 1599 Dec 09 to 2201 Feb 20 (JED 2305424.50 to JED 2525008.50)
This ephemeris was used for the Astronomical Almanac from 2003 to the present.
DE406Created May 1997; includes neither nutations nor librations.
Referred to the International Celestial Reference Frame.
A Long Ephemeris spanning -3001 Feb 04 to +3000 May 06 (JED 625360.5 to JED 2816912.5)
This is the same integration as DE405, with the accuracy of the interpolating polynomials has been lessened to reduce file size for the longer time span covered by the file.
DE430Created April 2013; includes librations and 1980 nutation.
Referred to the International Celestial Reference Frame version 2.0.
DE430 reportedly has the most accurate lunar ephemeris to day.
Covers 1549 Dec 21 to 2650 Jan 25 (JED 2287184.5 to JED 2688976.5).
DE431Created April 2013; includes librations and 1980 nutation.
Referred to the International Celestial Reference Frame version 2.0.
DE431 has a less accurate lunar ephemeris than DE430 but covers an enormous 30,000-year time span.
A Long Ephemeris covering -13200 Aug 15 to 17191 Mar 15 (JED -0.3100015.5 to JED 8000016.5).
DE430 and DE431 are described in the following document:
ipnpr.jpl.nasa.gov/progress_report/42-196/196C.pdf

Note: Portions of this page come from Wikipedia and the Jet Propulsion Lab.