AGI Technology Beyond Earth Orbit

CB Mu Values• Orbital element conversions–Uses the mu value from the *.cb file [Gm keyword]• TwoBody, J2Perturbation, J4Perturbation–Uses the mu value from the *.cb file• Propagation–mu and other values from the selected gravity file• Third Body Perturbations–Uses the System Mu value (if specified in *.cb file)AGIPg 23 of 40www.agi.com