Module: oeStateEphem¶

This module takes the TDB time, current object time and computes the state of the object using the time corrected by TDB and the stored Chebyshev coefficients.

If the time provided is outside the specified range for which the stored Chebyshev coefficients are valid then the position vectors rail high/low appropriately. More information can be found in the PDF Description.

Defines

MAX_OE_RECORDS¶

MAX_OE_COEFF¶

Functions

void SelfInit_oeStateEphem(OEStateEphemData *configData, int64_t moduleID)¶

This method creates the output navigation message (translation only) for the ephemeris model

Return

void

Parameters

configData: The configuration data associated with the ephemeris model
moduleID: The module identification integer

void CrossInit_oeStateEphem(OEStateEphemData *configData, int64_t moduleID)¶

This method initializes the input time correlation factor structure

Return

void

Parameters

configData: The configuration data associated with the ephemeris model
moduleID: The module identification integer

void Update_oeStateEphem(OEStateEphemData *configData, uint64_t callTime, int64_t moduleID)¶

This method takes the current time and computes the state of the object using that time and the stored Chebyshev coefficients. If the time provided is outside the specified range, the position vectors rail high/low appropriately.

Return

void

Parameters

configData: The configuration data associated with the ephemeris model
callTime: The clock time at which the function was called (nanoseconds)
moduleID: The module identification integer

void Reset_oeStateEphem(OEStateEphemData *configData, uint64_t callTime, int64_t moduleID)¶

This Reset method is empty

Return

void

Parameters

configData: The configuration data associated with the ephemeris model
callTime: The clock time at which the function was called (nanoseconds)
moduleID: The module identification integer

struct ChebyOERecord¶

#include <oeStateEphem.h>

Structure that defines the layout of an Ephemeris “record.” This is basically the set of coefficients for the ephemeris elements and the time factors associated with those coefficients.

Public Members

uint32_t nChebCoeff¶: [-] Number chebyshev coefficients loaded into record

double ephemTimeMid¶: [s] Ephemeris time (TDB) associated with the mid-point of the curve

double ephemTimeRad¶: [s] “Radius” of time that curve is valid for (half of total range

double rPeriapCoeff[MAX_OE_COEFF]¶: [-] Set of chebyshev coefficients for radius at periapses

double eccCoeff[MAX_OE_COEFF]¶: [-] Set of chebyshev coefficients for eccentrity

double incCoeff[MAX_OE_COEFF]¶: [-] Set of chebyshev coefficients for inclination

double argPerCoeff[MAX_OE_COEFF]¶: [-] Set of chebyshev coefficients for argument of periapses

double RAANCoeff[MAX_OE_COEFF]¶: [-] Set of chebyshev coefficients for right ascention of the ascending node

double anomCoeff[MAX_OE_COEFF]¶: [-] Set of chebyshev coefficients for true anomaly angle

uint32_t anomalyFlag¶: [-] Flag indicating if the anomaly angle is true (0), mean (1)

struct OEStateEphemData¶

#include <oeStateEphem.h>

Top level structure for the Chebyshev position ephemeris fit system. Allows the user to specify a set of chebyshev coefficients and then use the input time to determine where a given body is in space.

Public Members

char stateFitOutMsgName[MAX_STAT_MSG_LENGTH]¶: [-] The name of the output navigation message for pos/vel

char clockCorrInMsgName[MAX_STAT_MSG_LENGTH]¶: The name of the clock correlation message.

double muCentral¶: [m3/s^2] Gravitational parameter for center of orbital elements

ChebyOERecord ephArray[MAX_OE_RECORDS]¶: [-] Array of Chebyshev records for ephemeris

int32_t stateFitOutMsgId¶: [-] The ID associated with the outgoing message

int32_t clockCorrInMsgId¶: [-] The ID associated with the incoming clock correlation

uint32_t coeffSelector¶: [-] Index in the ephArray that we are currently using

BSKLogger *bskLogger¶: BSK Logging.