orb_data_s Struct Reference

Structure for storing orbit data.

List of all members.

Public Attributes
double	sma
	Semi-major axis [km].
double	inc
	Inclination [rad].
double	raan
	Right ascension of the ascending node [rad].
double	perigee
	Argument of perigee [rad].
double	ecc
	Eccentricity.
double	mean_anom
	Mean anomaly at epoch [rad].
double	true_anom
	True anomaly at epoch [rad].
double	orb_rate
	Mean orbit rate [rad/day].
double	epoch
	Epoch [Julian Days from J2000].

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Member Data Documentation

double orb_data_s::sma

Referenced by add_elements(), Alfriend2El(), El2Alfriend(), el_to_rv(), FFEccEstimateCost(), FFEccGenerateTeamGoals(), GenerateTimeVector(), GetHillsMats(), GVEErrorDynamics(), ImpulsiveLPManeuver(), ImpulsiveManeuver(), IterativeImpulsiveManeuver(), LPCircularTimeWeight(), LPEccentricGVE(), LPEccentricTimeWeight(), MonitoringAlg(), OrbElemDiff(), orbit_acquisition_dv(), rv_orb_gen(), rv_to_el(), and sub_elements().

double orb_data_s::inc

Referenced by add_elements(), Alfriend2El(), El2Alfriend(), el_to_rv(), GVEErrorDynamics(), ImpulsiveManeuver(), OrbElemDiff(), orbit_acquisition_dv(), rv_orb_gen(), rv_to_el(), and sub_elements().

double orb_data_s::raan

Referenced by add_elements(), Alfriend2El(), El2Alfriend(), el_to_rv(), OrbElemDiff(), orbit_acquisition_dv(), rv_orb_gen(), rv_to_el(), and sub_elements().

double orb_data_s::perigee

Referenced by add_elements(), Alfriend2El(), DeltaEl2AlfriendMat(), El2Alfriend(), el_to_rv(), FFEccGenerateTeamGoals(), GVEErrorDynamics(), ImpulsiveLPManeuver(), IterativeImpulsiveManeuver(), LPCircularTimeWeight(), MonitoringAlg(), OrbElemDiff(), orbit_acquisition_dv(), rv_orb_gen(), rv_to_el(), and sub_elements().

double orb_data_s::ecc

Referenced by add_elements(), Alfriend2El(), AutoFormGeometry(), DeltaEl2AlfriendMat(), El2Alfriend(), el_to_rv(), FFEccEstimateCost(), FFEccGenerateTeamGoals(), GenerateTimeVector(), GetHillsMats(), GVEErrorDynamics(), ImpulsiveLPManeuver(), ImpulsiveManeuver(), IterativeImpulsiveManeuver(), LPCircularTimeWeight(), LPEccentricGVE(), LPEccentricTimeWeight(), MonitoringAlg(), OrbElemDiff(), rv_orb_gen(), rv_to_el(), and sub_elements().

double orb_data_s::mean_anom

Referenced by add_elements(), Alfriend2El(), AutoFormGeometry(), DeltaEl2AlfriendMat(), El2Alfriend(), el_to_rv(), FFEccEstimateCost(), GenerateTimeVector(), GVEErrorDynamics(), ImpulsiveLPManeuver(), IterativeImpulsiveManeuver(), LPCircularTimeWeight(), LPEccentricGVE(), LPEccentricTimeWeight(), MonitoringAlg(), OrbElemDiff(), orbit_acquisition_dv(), rv_orb_gen(), rv_to_el(), sub_elements(), and galilean_moons::update().

double orb_data_s::true_anom

Referenced by add_elements(), Alfriend2El(), ECI2MeanElements(), FFEccHills2DeltaElem(), GetHillsMats(), OrbElemDiff(), rv_to_el(), and sub_elements().

double orb_data_s::orb_rate

Referenced by rv_to_el(), and galilean_moons::update().

double orb_data_s::epoch