TOMASuplNavigationModel Class Reference
class TOMASuplNavigationModel
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TOMASuplSatelliteInfoElement
holds values for
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GPS Week, which contains values for GPS Week of the Assistance Data currently held in the SET. The valid range is 0 to 1023.
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GPS Toe, which contains the GPS time of Ephemeris in hours of the newest set of Ephemeris contained in the SUPL Enabled Terminal. Valid range is 0 to 167.
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NSat, which contains the number of satellites to be considered for the current GPS Assistance data request. Valid range is 0 to 32.
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Toe Limit, which contains the Ephemeris age tolerance of the SUPL Enabled Terminal in hours. Valid range is 0 to 10.
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A list of Satellite Info objects. The number of satellite info elements held by the list is same as NSat. Each Satellite Info element contains the Satellite ID and Satellite Sequence Number.
Constructor & Destructor Documentation
TOMASuplNavigationModel()
IMPORT_C
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TOMASuplNavigationModel
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(
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)
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~TOMASuplNavigationModel()
IMPORT_C
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~TOMASuplNavigationModel
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(
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)
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Member Functions Documentation
GetNavigationModel(TInt &, TInt &, TInt &, TInt &)
IMPORT_C void
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GetNavigationModel
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(
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TInt
&
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aGpsWeek,
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TInt
&
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aGpsToe,
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TInt
&
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aNSAT,
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TInt
&
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aToeLimit
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)
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const
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GetNavigationModel retrieves values for the different parameters of Navigation Data.
Parameters
TInt
& aGpsWeek
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A reference parameter that holds the GPS Week of the assistance data currently held.
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TInt
& aGpsToe
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A reference parameter that holds the GPS Time of Ephemeris in hours of the newest set of Ephemeris.
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TInt
& aNSAT
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A reference parameter that holds Number of satellites to be considered for the current GPS assistance data request.
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TInt
& aToeLimit
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A reference parameter that holds T-Toe Limit, that contains the age tolerance of the SET to the network in hours.
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GetSatInfoElement(RArray< TOMASuplSatelliteInfoElement > &)
GetSatInfoElement(TOMASuplSatelliteInfoElement &, TInt)
GetSatInfoElement gets Satellite Info element at a given index
Parameters
TOMASuplSatelliteInfoElement
& aSatInfo
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A reference parameter that holds the Satellite Info Element
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TInt
aIndex
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The index for the Satellite Info Element to be retrieved
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SetNavigationModel(TInt, TInt, TInt, TInt)
SetNavigationModel sets values for the different parameters of Navigation Data
Parameters
TInt
aGpsWeek
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GPS Week of the assistance data currently held. Valid range is 0 to 1023
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TInt
aGpsToe
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GPS Time of Ephemeris in hours of the newest set of Ephemeris. Valid range is 0 to 167
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TInt
aNSAT
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Number of satellites to be considered for the current GPS assistance data request. Valid range is 0 to 31. If the SUPL Enabled Terminal has no ephemeris data, this field shall be set to zero. If the SUPL Enabled Terminal has ephemeris data whose age exceeds the T-Toe Limit, this field may be set to zero. If the network receives a zero value for this field, it ignores the GPS Week, GPS Toe fields and assumes that the SUPL Enabled Terminal has no ephemeris value
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TInt
aToeLimit
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T-Toe Limit, that contains the age tolerance of the SET to the network in hours. Valid range is 0 to 10.
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SetSatInfoElement(const RArray< TOMASuplSatelliteInfoElement > &)
SetSatInfoElement sets the Satellite Info Elements
SetSatInfoElement(const TOMASuplSatelliteInfoElement &, TInt)
SetSatInfoElement sets Satellite Info element at a given index
Parameters
const
TOMASuplSatelliteInfoElement
& aSatInfo
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Parameter that holds the Satellite Info Element
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TInt
aIndex
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The index at which the Satellite Info element has to be set
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operator=(const TOMASuplNavigationModel &)
Member Data Documentation
RArray< TOMASuplSatelliteInfoElement > iSatInfo
TBool
iSatInfoPresent
TBool
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iSatInfoPresent
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[private]
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Copyright ©2010 Nokia Corporation and/or its subsidiary(-ies).
All rights
reserved. Unless otherwise stated, these materials are provided under the terms of the Eclipse Public License
v1.0.