- Eccentric anomaly
The eccentric anomaly is the angle between the direction of
periapsis and the current position of an object on itsorbit , projected onto the ellipse's circumscribing circle perpendicularly to the major axis, measured at the centre of theellipse . In the diagram below, it is E (the angle zcx).Calculation
In
astrodynamics eccentric anomaly "E" can be calculated as follows::
where:
* is the orbiting body's position vector (segment "sp"),
* is the orbit'ssemi-major axis (segment "cz"), and
* is the orbit's eccentricity.The relation between "E" and "M", the
mean anomaly , is::
This equation can be solved iteratively, starting from and using the relation .
The equation can also be expanded in powers of , as long as . The first few terms of the expansion are:
*
*
* .For references on details of this derivation, as well as other more efficient methods of solution, see Murray and Dermott (1999, p.35). For a derivation of the limiting value of see Plummer (1960, section 46).The relation between "E" and "ν", the
true anomaly , is::
or equivalently
:
The relations between the radius (position vector magnitude) and the anomalies are:
:
and
:
ee also
*
Kepler's laws of planetary motion
*Mean anomaly
*True anomaly References
* Murray, C. D. & Dermott, S. F. 1999, Solar System Dynamics, Cambridge University Press, Cambridge.
* Plummer, H.C., 1960, An Introductory treatise on Dynamical Astronomy, Dover Publications, New York. (Reprint of the 1918 Cambridge University Press edition.)
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