D H said:
You used the word "focus". What other than Keplerian orbits have foci?
Humankind have been sending objects to other solar system bodies for fifty years and have been doing high precision solar system astronomy for well over fifty years. That's plenty of time to learn how to do it best, where "best" means predicting the vehicle will go with minimal error, or predicting where to point that high-precision telescope such that the desired object is in its field of view. In this context, "best" is very clear: Completely toss the notion of Keplerian orbits, and that includes your notion of a "primary focus". It turns out that using a barycentric frame using cartesian equations of motion and geometric integrators does a much, much better job than does using a heliocentric frame with perturbed Keplerian orbits.
A barycentric frame only means the use of that
mathematical point as the basis for a coordinate system. True?
If a heliocentric frame means the use of a
mathematical point that
begins near the center of the Sun then the results are going to be comparable. True? If a helocentric frame means the frame is moving with the center of the Sun then the results will not be automatically comparable.
It was never my intention to say the Earth system has the center of the sun as the orbital center, however according to JPL the best available ephemerides show this is approximately true where the Earth Sun distance is 'constant' over large numbers of years. The same applies for the distance of the other planets from the Sun.
To be honest i am not sure what you are getting at here.
This thread has already covered all the points raised in the argument i was having. The conversation was not so advanced that we were talking about sending vehicles to Neptune or needing to know more than Newton would know. Additionally prior to 1984, the best available ephemerides for the inner planets (excluding Earth?) used 1898 methodology, and as of at least 2004 GPS satellites were still being sent ephemerides that are 'keplerian in nature'.
reference. From JPL.NASA. URL no longer working (http://iau-comm4.jpl.nasa.gov/XSChap8.pdf
CHAPTER 8: Orbital Ephemerides of the Sun, Moon, and Planets
E. Myles Standish and James G. Williams
8.1 Fundamental Ephemerides
The fundamental planetary and lunar ephemerides of The Astronomical Almanac, starting in the year 2003, are DE405/LE405of Caltech’s Jet Propulsion Laboratory (JPL). They replace JPL’s DE200 which have been used in the almanac since 1984. Previous to 1984, the fundamental ephemerides were based upon analytical “theories”; these are described in
Section 8.2.
8.2 Previous Ephemerides used in the Astronomical Almanacs
8.2.1 Ephemerides Prior to 1984
Before 1984, the ephemerides for the Sun, Mercury, Venus, and Mars were based on the theories and tables of Newcomb (1898). Computerized evaluations of the tables were used from 1960 through 1980. From 1981 to 1983, the ephemerides were based on the evaluations of the theories themselves. The ephemerides of the Sun were derived from the algorithm given by S. Newcomb in Tables of the Sun (Newcomb, 1898). Newcomb’s theories of the inner planets (1895–1898) served as the basis for the heliocentric ephemerides of Mercury, Venus, and Mars. In the case of Mars, the corrections derived by F.E. Ross (1917) were applied.
Ephemerides of the outer planets, Jupiter, Saturn, Uranus, Neptune, and Pluto, were computed from the heliocentric rectangular coordinates obtained by numerical integration (Eckert et al., 1951).