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https://github.com/Evolution-X/hardware_interfaces
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Merge "Change TOC and TOE to long" into tm-dev
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Android (Google) Code Review
commit
f268ae2cef
@@ -40,10 +40,10 @@ parcelable SatellitePvt {
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android.hardware.gnss.SatelliteClockInfo satClockInfo;
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double ionoDelayMeters;
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double tropoDelayMeters;
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int TOC;
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int IODC;
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int TOE;
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int IODE;
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long timeOfClockSeconds;
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int issueOfDataClock;
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long timeOfEphemerisSeconds;
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int issueOfDataEphemeris;
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android.hardware.gnss.SatellitePvt.SatelliteEphemerisSource ephemerisSource = android.hardware.gnss.SatellitePvt.SatelliteEphemerisSource.OTHER;
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const int HAS_POSITION_VELOCITY_CLOCK_INFO = 1;
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const int HAS_IONO = 2;
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@@ -76,12 +76,13 @@ parcelable SatellitePvt {
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double tropoDelayMeters;
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/**
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* Time of Clock.
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* Time of Clock in seconds.
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*
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* This is defined in GPS ICD200 documentation
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* (e.g., https://www.gps.gov/technical/icwg/IS-GPS-200H.pdf).
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* This value is defined in seconds since GPS epoch, regardless of the constellation.
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*
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* The value must not be encoded as in GPS ICD200 documentation.
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*/
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int TOC;
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long timeOfClockSeconds;
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/**
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* Issue of Data, Clock.
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@@ -91,15 +92,16 @@ parcelable SatellitePvt {
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*
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* The field must be set to 0 if it is not supported.
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*/
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int IODC;
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int issueOfDataClock;
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/**
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* Time of Ephemeris.
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* Time of Ephemeris in seconds.
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*
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* This is defined in GPS ICD200 documentation
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* (e.g., https://www.gps.gov/technical/icwg/IS-GPS-200H.pdf).
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* This value is defined in seconds since GPS epoch, regardless of the constellation.
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*
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* The value must not be encoded as in GPS ICD200 documentation.
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*/
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int TOE;
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long timeOfEphemerisSeconds;
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/**
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* Issue of Data, Ephemeris.
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@@ -109,7 +111,7 @@ parcelable SatellitePvt {
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*
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* The field must be set to 0 if it is not supported.
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*/
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int IODE;
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int issueOfDataEphemeris;
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/** Satellite's ephemeris source */
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@VintfStability
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@@ -366,12 +366,13 @@ void CheckSatellitePvt(const SatellitePvt& satellitePvt, const int interfaceVers
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ASSERT_TRUE(satellitePvt.tropoDelayMeters > 0 && satellitePvt.tropoDelayMeters < 100);
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}
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if (interfaceVersion >= 2) {
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ASSERT_TRUE(satellitePvt.TOC >= 0 && satellitePvt.TOC <= 604784);
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ASSERT_TRUE(satellitePvt.TOE >= 0 && satellitePvt.TOE <= 604784);
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ASSERT_TRUE(satellitePvt.timeOfClockSeconds >= 0);
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ASSERT_TRUE(satellitePvt.timeOfEphemerisSeconds >= 0);
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// IODC has 10 bits
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ASSERT_TRUE(satellitePvt.IODC >= 0 && satellitePvt.IODC <= 1023);
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ASSERT_TRUE(satellitePvt.issueOfDataClock >= 0 && satellitePvt.issueOfDataClock <= 1023);
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// IODE has 8 bits
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ASSERT_TRUE(satellitePvt.IODE >= 0 && satellitePvt.IODE <= 255);
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ASSERT_TRUE(satellitePvt.issueOfDataEphemeris >= 0 &&
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satellitePvt.issueOfDataEphemeris <= 255);
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}
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}
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@@ -201,10 +201,10 @@ GnssData Utils::getMockMeasurement(const bool enableCorrVecOutputs) {
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.tropoDelayMeters = 3.882265204404031,
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.ephemerisSource =
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SatellitePvt::SatelliteEphemerisSource::SERVER_LONG_TERM,
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.TOC = 12345,
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.IODC = 143,
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.TOE = 9876,
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.IODE = 48,
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.timeOfClockSeconds = 12345,
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.issueOfDataClock = 143,
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.timeOfEphemerisSeconds = 9876,
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.issueOfDataEphemeris = 48,
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},
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.correlationVectors = {}};
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