matlab documentation

doc.m

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%   Purpose: 
%       - Function that loads planetary constant values for AAE532 class
%
%   Inputs: 
%       - none
%
%   Outpus: 
%       - constants - structure that holds constants for sol system divided
%       by body
%           - rot_per - axial rotational period in rev/day
%           - radius - mean equatorial radius in km
%           - mu - graviational parameter in km^3/sec^2
%           - orbit_sma - semi-major axis of orbit in km
%           - orbit_per - period of orbit in sec
%           - orbit_ecc - eccentricity of orbit
%           - orbit_inc - inclination of orbit in deg
%           - mass - body mass (derived from mu and G) in kg
%           - G - universal graviational constant in km^3/kg*sec^2
%
%   Dependencies: 
%       - none
%
%   Author: 
%       - Shankar Kulumani 1 Sept 2012
%           - list revisions
%       - Shankar Kulumani 19 Sept 2012
%           - added distance conversions
%           - added time conversions
%       - Shankar Kulumani 30 Oct 2012
%           - added semiparamter to constants
%
%   References
%       - planetary_constants.pdf (from AAE532 supplements)	
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