Module: oeStateEphem
Executive Summary
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
.
Message Connection Descriptions
The following table lists all the module input and output messages. The module msg connection is set by the user from python. The msg type contains a link to the message structure definition, while the description provides information on what this message is used for.
Msg Variable Name |
Msg Type |
Description |
---|---|---|
stateFitOutMsg |
output navigation message for pos/vel |
|
clockCorrInMsg |
clock correlation input message |
Functions
-
void SelfInit_oeStateEphem(OEStateEphemData *configData, int64_t moduleID)
This method creates the output navigation message (translation only) for the ephemeris model
- Parameters:
configData – The configuration data associated with the ephemeris model
moduleID – The module identification integer
- Returns:
void
-
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.
- 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
- Returns:
void
-
void Reset_oeStateEphem(OEStateEphemData *configData, uint64_t callTime, int64_t moduleID)
This Reset method is empty
- 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
- Returns:
void
-
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)
-
uint32_t nChebCoeff
-
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
-
EphemerisMsg_C stateFitOutMsg
[-] output navigation message for pos/vel
-
TDBVehicleClockCorrelationMsg_C clockCorrInMsg
clock correlation input message
-
double muCentral
[m3/s^2] Gravitational parameter for center of orbital elements
-
ChebyOERecord ephArray[MAX_OE_RECORDS]
[-] Array of Chebyshev records for ephemeris
-
uint32_t coeffSelector
[-] Index in the ephArray that we are currently using
-
BSKLogger *bskLogger
BSK Logging.
-
EphemerisMsg_C stateFitOutMsg