Moon Perturbation - Argument of Perigee

Not Reviewed
Equation / Last modified by Administrator on 2015/08/11 07:07
`dotomega_"Moon" = `
Rating
ID
MichaelBartmess.Moon Perturbation - Argument of Perigee
UUID
0bbe2f83-ed22-11e3-b7aa-bc764e2038f2

This equation computes the rate of change of the argument of perigee, `dotomega`, of an orbit where the rate of change in deg/day results from the Moon's third-body gravitational influence on the orbit.  The inputs to this equation are the orbit inclination (i) and the number of orbit revolutions per day (n).

 

MoonPerturbationArgumentofPerigee-illustration.png

Notes

This computation is an approximation, as it neglects the perturbation caused by the change in orientation of the orbital plane relative to the Moon's orbital plane.