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Earth Observation Mission CFI Software Orbit Software User Manual |
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Earth Observation Mission CFI Software Orbit Software User Manual |
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This class contains a time instant given as an absolute orbit number plus the time elapsed since the ANX. More...
Public Member Functions | |
| ANXTime () | |
| Class constructor. | |
| ANXTime (long orbitIn, long secondsIn, long microsecIn) | |
| Class constructor with AXN time. | |
| ANXTime (const OrbitId &orbitId, long orbitIn, long secondsIn, long microsecIn) throw (CfiError) | |
| Class constructor with ANX time and Orbit id. | |
| ANXTime (const ANXTime &at) | |
| Copy constructor. | |
| ~ANXTime () | |
| Class destructor. | |
| double | orbitToTime (long timeRef) const throw (CfiError) |
| Compute the time for a given orbit and time after the ANX. | |
| void | timeToOrbit (long timeRef, double time) throw (CfiError) |
| Get the absolute orbit number and the time after the ANX for a given time. | |
| void | setBOM () |
| Set time to Beggining of mission (BOM). | |
| void | setEOM () |
| Set time to End of mission (EOM). | |
| OrbitalInfo | getOrbitInfo () const throw (CfiError) |
| Returns orbital information for the orbit of the object. | |
| void | orbitInfoConfigure (long item, long option) const throw (CfiError) |
| Method that can be used to activate/deactivate the computation of several parameters in call to ANXTime::getOrbitInfo. | |
| void | adjustWithNodalPeriod () throw (CfiError) |
| Correct ANX time taking into account the orbit duration. | |
| ANXTime | operator+ (double time) |
| Operator + (add a time). | |
| ANXTime | operator- (double time) |
| Operator - (subtract a time). | |
| double | operator- (const ANXTime &t) const throw (CfiError) |
| Substract two ANXTime objects and returns the number of seconds between them. | |
| bool | operator> (const ANXTime &t) const throw (CfiError) |
| Operator > . | |
| bool | operator< (const ANXTime &t) const throw (CfiError) |
| Operator < . | |
| bool | operator>= (const ANXTime &t) const throw (CfiError) |
| Operator >= . | |
| bool | operator<= (const ANXTime &t) const throw (CfiError) |
| Operator <= . | |
| bool | operator== (const ANXTime &t) const throw (CfiError) |
| Operator ==. | |
| bool | operator!= (const ANXTime &t) const throw (CfiError) |
| Operator != . | |
| void | operator= (const ANXTime &t) |
| Assigment operator. | |
Public Attributes | |
| long | orbit |
| Absolute orbit number. | |
| long | seconds |
| Seconds since the ANX. | |
| long | microseconds |
| Microseconds. | |
This class contains a time instant given as an absolute orbit number plus the time elapsed since the ANX.
| EECFI::ANXTime::ANXTime | ( | ) |
Class constructor.
| EECFI::ANXTime::ANXTime | ( | long | orbitIn, | |
| long | secondsIn, | |||
| long | microsecIn | |||
| ) |
Class constructor with AXN time.
References microseconds, orbit, and seconds.
| EECFI::ANXTime::ANXTime | ( | const OrbitId & | orbitId, | |
| long | orbitIn, | |||
| long | secondsIn, | |||
| long | microsecIn | |||
| ) | throw (CfiError) |
Class constructor with ANX time and Orbit id.
| EECFI::ANXTime::ANXTime | ( | const ANXTime & | at | ) |
Copy constructor.
| at | ANXTime object to copy. |
References microseconds, orbit, and seconds.
| EECFI::ANXTime::~ANXTime | ( | ) |
Class destructor.
| void EECFI::ANXTime::adjustWithNodalPeriod | ( | ) | throw (CfiError) |
Correct ANX time taking into account the orbit duration.
References EECFI::CfiError::addMsg(), getOrbitInfo(), microseconds, EECFI::OrbitalInfo::nodalPeriod, orbit, and seconds.
Referenced by operator-(), operator<(), operator==(), and operator>().
| OrbitalInfo EECFI::ANXTime::getOrbitInfo | ( | ) | const throw (CfiError) |
Returns orbital information for the orbit of the object.
References EECFI::OrbitalInfo::absOrbit, EECFI::CfiError::addMsg(), EECFI::OrbitalInfo::cycLength, EECFI::OrbitalInfo::meanKep, EECFI::OrbitalInfo::mlst, EECFI::OrbitalInfo::mlstDrift, EECFI::OrbitalInfo::nodalPeriod, orbit, EECFI::OrbitalInfo::oscKep, EECFI::OrbitalInfo::phasing, EECFI::OrbitalInfo::posAnx, EECFI::OrbitalInfo::repCycle, EECFI::CfiClass::throwWarn, EECFI::OrbitalInfo::utcAnx, EECFI::OrbitalInfo::utcSmx, and EECFI::OrbitalInfo::velAnx.
Referenced by adjustWithNodalPeriod(), and operator-().
Operator != .
| at | ANXTime object we want to compare with. |
References EECFI::CfiError::addMsg().
| ANXTime EECFI::ANXTime::operator+ | ( | double | time | ) |
Operator + (add a time).
| time | Seconds to be added to the ANXTime object. |
References microseconds, and seconds.
| ANXTime EECFI::ANXTime::operator- | ( | double | time | ) |
Operator - (subtract a time).
| time | Seconds to be substracted from the ANXTime object. |
References microseconds, and seconds.
Substract two ANXTime objects and returns the number of seconds between them.
| at | ANXTime object we want to substract to the object. |
References EECFI::CfiError::addMsg(), adjustWithNodalPeriod(), getOrbitInfo(), microseconds, EECFI::OrbitalInfo::nodalPeriod, orbit, and seconds.
Operator < .
| at | ANXTime object we want to compare with. |
References EECFI::CfiError::addMsg(), adjustWithNodalPeriod(), microseconds, orbit, and seconds.
Operator <= .
| at | ANXTime object we want to compare with. |
References EECFI::CfiError::addMsg().
| void EECFI::ANXTime::operator= | ( | const ANXTime & | t | ) |
Assigment operator.
| t | ANXTime object we want to copy values into this one. |
References microseconds, orbit, and seconds.
Operator ==.
| at | ANXTime object we want to compare with. |
References EECFI::CfiError::addMsg(), adjustWithNodalPeriod(), microseconds, orbit, and seconds.
Operator > .
| at | ANXTime object we want to compare with. |
References EECFI::CfiError::addMsg(), adjustWithNodalPeriod(), microseconds, orbit, and seconds.
Operator >= .
| at | ANXTime object we want to compare with. |
References EECFI::CfiError::addMsg().
| void EECFI::ANXTime::orbitInfoConfigure | ( | long | item, | |
| long | option | |||
| ) | const throw (CfiError) |
Method that can be used to activate/deactivate the computation of several parameters in call to ANXTime::getOrbitInfo.
Some parameters computed by ANXTime::getOrbitInfo require a significant computation time, so their computation is disabled by default and must be activated with orbitInfoConfigure method. The parameters that can be activated currently are the following ones:
| item | Orbit info item to be activated/deactivated (OrbitInfoItemsEnum). | |
| option | Activate/deactivate item computation (OrbitInfoFlagEnum). |
| double EECFI::ANXTime::orbitToTime | ( | long | timeRef | ) | const throw (CfiError) |
Compute the time for a given orbit and time after the ANX.
| timeRef | Time reference (TimeRefOrbitEnum). |
References EECFI::CfiError::addMsg().
| void EECFI::ANXTime::setBOM | ( | ) |
Set time to Beggining of mission (BOM).
| void EECFI::ANXTime::setEOM | ( | ) |
Set time to End of mission (EOM).
| void EECFI::ANXTime::timeToOrbit | ( | long | timeRef, | |
| double | time | |||
| ) | throw (CfiError) |
Get the absolute orbit number and the time after the ANX for a given time.
Results are stored in the object.
References EECFI::CfiError::addMsg().
Microseconds.
Referenced by adjustWithNodalPeriod(), ANXTime(), operator+(), operator-(), operator<(), operator=(), operator==(), operator>(), and EECFI::RelANXTime::toAbsolute().
Absolute orbit number.
Referenced by adjustWithNodalPeriod(), ANXTime(), getOrbitInfo(), operator-(), operator<(), operator=(), operator==(), operator>(), and EECFI::RelANXTime::toAbsolute().
Seconds since the ANX.
Referenced by adjustWithNodalPeriod(), ANXTime(), operator+(), operator-(), operator<(), operator=(), operator==(), operator>(), and EECFI::RelANXTime::toAbsolute().
1.7.1