AST352L--Spring 1998
Determining the Position of a Comet
1. Within the Orbital Plane
This assignment is DUE on Wednesday, April 8.
The elements of the orbit of Comet Encke are
- a=2.2091401 AU
- e=0.8502196
- I=11.94524°
- Longitude of Node (Big Omega)=334.75006°
- Argument of Perihelion (little omega)=186.23352°
- T=1990 October 28.54502, Dynamical Time
Determine the following for the position of the comet within the orbital
plane, for the date 1990 October 5.0 Dynamical Time.
- The mean motion n.
- The mean anomaly, l.
- The eccentric anomaly, u.
- The true anomaly, f.
- The radius r , using both the formula in f and the formula
in u.
- The (x,y ) position of the comet in the orbital plane, using
the formulas in u.
- The (x,y ) position of the comet in the orbital plane, using
the forumlas in f (should agree with the previous result).
- The components (xdot, ydot) of the velocity of the comet in
the orbital plane, using the formulas in u.
- The components (xdot, ydot) of the velocity of the comet in
the orbital plane, using the hodograph formula (should agree with the previous
result).
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