Files
frameworks_base/location/java/android/location/GnssMeasurement.java
Yu-Han Yang 9fe06ddab8 Add basebandCn0Dbhz to GnssMeasurement
The new basebandCn0DbHz is the carrier-to-noise density measured at the
baseband. The old Cn0DbHz is measured at the attenna port. Adding
the new field so that ecosystem will report both and avoid reporting
inconsistent signal strengths in one field. See go/r-gnss-hal for
detailed design.

Bug: 136136192
Test: atest GnssMeasurementTest
Change-Id: Ia8d3711e7422db5cae05d66138a3fae61bec0ae1
2019-11-26 14:29:07 -08:00

1610 lines
54 KiB
Java

/*
* Copyright (C) 2014 The Android Open Source Project
*
* Licensed under the Apache License, Version 2.0 (the "License");
* you may not use this file except in compliance with the License.
* You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License
*/
package android.location;
import android.annotation.FloatRange;
import android.annotation.IntDef;
import android.annotation.NonNull;
import android.annotation.TestApi;
import android.hardware.gnss.V1_0.IGnssMeasurementCallback.GnssMeasurementFlags;
import android.os.Parcel;
import android.os.Parcelable;
import java.lang.annotation.Retention;
import java.lang.annotation.RetentionPolicy;
/**
* A class representing a GNSS satellite measurement, containing raw and computed information.
*/
public final class GnssMeasurement implements Parcelable {
private int mFlags;
private int mSvid;
private int mConstellationType;
private double mTimeOffsetNanos;
private int mState;
private long mReceivedSvTimeNanos;
private long mReceivedSvTimeUncertaintyNanos;
private double mCn0DbHz;
private double mBasebandCn0DbHz;
private double mPseudorangeRateMetersPerSecond;
private double mPseudorangeRateUncertaintyMetersPerSecond;
private int mAccumulatedDeltaRangeState;
private double mAccumulatedDeltaRangeMeters;
private double mAccumulatedDeltaRangeUncertaintyMeters;
private float mCarrierFrequencyHz;
private long mCarrierCycles;
private double mCarrierPhase;
private double mCarrierPhaseUncertainty;
private int mMultipathIndicator;
private double mSnrInDb;
private double mAutomaticGainControlLevelInDb;
@NonNull private String mCodeType;
// The following enumerations must be in sync with the values declared in GNSS HAL.
private static final int HAS_NO_FLAGS = 0;
private static final int HAS_SNR = GnssMeasurementFlags.HAS_SNR;
private static final int HAS_CARRIER_FREQUENCY = GnssMeasurementFlags.HAS_CARRIER_FREQUENCY;
private static final int HAS_CARRIER_CYCLES = GnssMeasurementFlags.HAS_CARRIER_CYCLES;
private static final int HAS_CARRIER_PHASE = GnssMeasurementFlags.HAS_CARRIER_PHASE;
private static final int HAS_CARRIER_PHASE_UNCERTAINTY =
GnssMeasurementFlags.HAS_CARRIER_PHASE_UNCERTAINTY;
private static final int HAS_AUTOMATIC_GAIN_CONTROL =
GnssMeasurementFlags.HAS_AUTOMATIC_GAIN_CONTROL;
private static final int HAS_CODE_TYPE = (1 << 14);
private static final int HAS_BASEBAND_CN0 = (1 << 15);
/**
* The status of the multipath indicator.
* @hide
*/
@Retention(RetentionPolicy.SOURCE)
@IntDef({MULTIPATH_INDICATOR_UNKNOWN, MULTIPATH_INDICATOR_DETECTED,
MULTIPATH_INDICATOR_NOT_DETECTED})
public @interface MultipathIndicator {}
/**
* The indicator is not available or the presence or absence of multipath is unknown.
*/
public static final int MULTIPATH_INDICATOR_UNKNOWN = 0;
/**
* The measurement shows signs of multi-path.
*/
public static final int MULTIPATH_INDICATOR_DETECTED = 1;
/**
* The measurement shows no signs of multi-path.
*/
public static final int MULTIPATH_INDICATOR_NOT_DETECTED = 2;
/**
* GNSS measurement tracking loop state
* @hide
*/
@IntDef(flag = true, prefix = { "STATE_" }, value = {
STATE_CODE_LOCK, STATE_BIT_SYNC, STATE_SUBFRAME_SYNC,
STATE_TOW_DECODED, STATE_MSEC_AMBIGUOUS, STATE_SYMBOL_SYNC, STATE_GLO_STRING_SYNC,
STATE_GLO_TOD_DECODED, STATE_BDS_D2_BIT_SYNC, STATE_BDS_D2_SUBFRAME_SYNC,
STATE_GAL_E1BC_CODE_LOCK, STATE_GAL_E1C_2ND_CODE_LOCK, STATE_GAL_E1B_PAGE_SYNC,
STATE_SBAS_SYNC, STATE_TOW_KNOWN, STATE_GLO_TOD_KNOWN, STATE_2ND_CODE_LOCK
})
@Retention(RetentionPolicy.SOURCE)
public @interface State {}
/** This GNSS measurement's tracking state is invalid or unknown. */
public static final int STATE_UNKNOWN = 0;
/** This GNSS measurement's tracking state has code lock. */
public static final int STATE_CODE_LOCK = (1<<0);
/** This GNSS measurement's tracking state has bit sync. */
public static final int STATE_BIT_SYNC = (1<<1);
/** This GNSS measurement's tracking state has sub-frame sync. */
public static final int STATE_SUBFRAME_SYNC = (1<<2);
/** This GNSS measurement's tracking state has time-of-week decoded. */
public static final int STATE_TOW_DECODED = (1<<3);
/** This GNSS measurement's tracking state contains millisecond ambiguity. */
public static final int STATE_MSEC_AMBIGUOUS = (1<<4);
/** This GNSS measurement's tracking state has symbol sync. */
public static final int STATE_SYMBOL_SYNC = (1<<5);
/** This Glonass measurement's tracking state has string sync. */
public static final int STATE_GLO_STRING_SYNC = (1<<6);
/** This Glonass measurement's tracking state has time-of-day decoded. */
public static final int STATE_GLO_TOD_DECODED = (1<<7);
/** This Beidou measurement's tracking state has D2 bit sync. */
public static final int STATE_BDS_D2_BIT_SYNC = (1<<8);
/** This Beidou measurement's tracking state has D2 sub-frame sync. */
public static final int STATE_BDS_D2_SUBFRAME_SYNC = (1<<9);
/** This Galileo measurement's tracking state has E1B/C code lock. */
public static final int STATE_GAL_E1BC_CODE_LOCK = (1<<10);
/** This Galileo measurement's tracking state has E1C secondary code lock. */
public static final int STATE_GAL_E1C_2ND_CODE_LOCK = (1<<11);
/** This Galileo measurement's tracking state has E1B page sync. */
public static final int STATE_GAL_E1B_PAGE_SYNC = (1<<12);
/** This SBAS measurement's tracking state has whole second level sync. */
public static final int STATE_SBAS_SYNC = (1<<13);
/**
* This GNSS measurement's tracking state has time-of-week known, possibly not decoded
* over the air but has been determined from other sources. If TOW decoded is set then TOW Known
* will also be set.
*/
public static final int STATE_TOW_KNOWN = (1<<14);
/**
* This Glonass measurement's tracking state has time-of-day known, possibly not decoded
* over the air but has been determined from other sources. If TOD decoded is set then TOD Known
* will also be set.
*/
public static final int STATE_GLO_TOD_KNOWN = (1<<15);
/** This GNSS measurement's tracking state has secondary code lock. */
public static final int STATE_2ND_CODE_LOCK = (1 << 16);
/**
* All the GNSS receiver state flags, for bit masking purposes (not a sensible state for any
* individual measurement.)
*/
private static final int STATE_ALL = 0x3fff; // 2 bits + 4 bits + 4 bits + 4 bits = 14 bits
/**
* GNSS measurement accumulated delta range state
* @hide
*/
@IntDef(flag = true, prefix = { "ADR_STATE_" }, value = {
ADR_STATE_VALID, ADR_STATE_RESET, ADR_STATE_CYCLE_SLIP, ADR_STATE_HALF_CYCLE_RESOLVED,
ADR_STATE_HALF_CYCLE_REPORTED
})
@Retention(RetentionPolicy.SOURCE)
public @interface AdrState {}
/**
* The state of the value {@link #getAccumulatedDeltaRangeMeters()} is invalid or unknown.
*/
public static final int ADR_STATE_UNKNOWN = 0;
/**
* The state of the {@link #getAccumulatedDeltaRangeMeters()} is valid.
*/
public static final int ADR_STATE_VALID = (1<<0);
/**
* The state of the {@link #getAccumulatedDeltaRangeMeters()} has detected a reset.
*/
public static final int ADR_STATE_RESET = (1<<1);
/**
* The state of the {@link #getAccumulatedDeltaRangeMeters()} has a cycle slip detected.
*/
public static final int ADR_STATE_CYCLE_SLIP = (1<<2);
/**
* Reports whether the value {@link #getAccumulatedDeltaRangeMeters()} has resolved the half
* cycle ambiguity.
*
* <p> When this bit is set, the {@link #getAccumulatedDeltaRangeMeters()} corresponds to the
* carrier phase measurement plus an accumulated integer number of carrier full cycles.
*
* <p> When this bit is unset, the {@link #getAccumulatedDeltaRangeMeters()} corresponds to the
* carrier phase measurement plus an accumulated integer number of carrier half cycles.
*/
public static final int ADR_STATE_HALF_CYCLE_RESOLVED = (1<<3);
/**
* Reports whether the flag {@link #ADR_STATE_HALF_CYCLE_RESOLVED} has been reported by the
* GNSS hardware.
*
* <p> When this bit is set, the value of {@link #getAccumulatedDeltaRangeUncertaintyMeters()}
* can be low (centimeter level) whether or not the half cycle ambiguity is resolved.
*
* <p> When this bit is unset, the value of {@link #getAccumulatedDeltaRangeUncertaintyMeters()}
* is larger, to cover the potential error due to half cycle ambiguity being unresolved.
*/
public static final int ADR_STATE_HALF_CYCLE_REPORTED = (1<<4);
/**
* All the 'Accumulated Delta Range' flags.
* @hide
*/
@TestApi
public static final int ADR_STATE_ALL =
ADR_STATE_VALID | ADR_STATE_RESET | ADR_STATE_CYCLE_SLIP |
ADR_STATE_HALF_CYCLE_RESOLVED | ADR_STATE_HALF_CYCLE_REPORTED;
// End enumerations in sync with gps.h
/**
* @hide
*/
@TestApi
public GnssMeasurement() {
initialize();
}
/**
* Sets all contents to the values stored in the provided object.
* @hide
*/
@TestApi
public void set(GnssMeasurement measurement) {
mFlags = measurement.mFlags;
mSvid = measurement.mSvid;
mConstellationType = measurement.mConstellationType;
mTimeOffsetNanos = measurement.mTimeOffsetNanos;
mState = measurement.mState;
mReceivedSvTimeNanos = measurement.mReceivedSvTimeNanos;
mReceivedSvTimeUncertaintyNanos = measurement.mReceivedSvTimeUncertaintyNanos;
mCn0DbHz = measurement.mCn0DbHz;
mBasebandCn0DbHz = measurement.mBasebandCn0DbHz;
mPseudorangeRateMetersPerSecond = measurement.mPseudorangeRateMetersPerSecond;
mPseudorangeRateUncertaintyMetersPerSecond =
measurement.mPseudorangeRateUncertaintyMetersPerSecond;
mAccumulatedDeltaRangeState = measurement.mAccumulatedDeltaRangeState;
mAccumulatedDeltaRangeMeters = measurement.mAccumulatedDeltaRangeMeters;
mAccumulatedDeltaRangeUncertaintyMeters =
measurement.mAccumulatedDeltaRangeUncertaintyMeters;
mCarrierFrequencyHz = measurement.mCarrierFrequencyHz;
mCarrierCycles = measurement.mCarrierCycles;
mCarrierPhase = measurement.mCarrierPhase;
mCarrierPhaseUncertainty = measurement.mCarrierPhaseUncertainty;
mMultipathIndicator = measurement.mMultipathIndicator;
mSnrInDb = measurement.mSnrInDb;
mAutomaticGainControlLevelInDb = measurement.mAutomaticGainControlLevelInDb;
mCodeType = measurement.mCodeType;
}
/**
* Resets all the contents to its original state.
* @hide
*/
@TestApi
public void reset() {
initialize();
}
/**
* Gets the satellite ID.
*
* <p>Interpretation depends on {@link #getConstellationType()}.
* See {@link GnssStatus#getSvid(int)}.
*/
public int getSvid() {
return mSvid;
}
/**
* Sets the Satellite ID.
* @hide
*/
@TestApi
public void setSvid(int value) {
mSvid = value;
}
/**
* Gets the constellation type.
*
* <p>The return value is one of those constants with {@code CONSTELLATION_} prefix in
* {@link GnssStatus}.
*/
@GnssStatus.ConstellationType
public int getConstellationType() {
return mConstellationType;
}
/**
* Sets the constellation type.
* @hide
*/
@TestApi
public void setConstellationType(@GnssStatus.ConstellationType int value) {
mConstellationType = value;
}
/**
* Gets the time offset at which the measurement was taken in nanoseconds.
*
* <p>The reference receiver's time from which this is offset is specified by
* {@link GnssClock#getTimeNanos()}.
*
* <p>The sign of this value is given by the following equation:
* <pre>
* measurement time = TimeNanos + TimeOffsetNanos</pre>
*
* <p>The value provides an individual time-stamp for the measurement, and allows sub-nanosecond
* accuracy.
*/
public double getTimeOffsetNanos() {
return mTimeOffsetNanos;
}
/**
* Sets the time offset at which the measurement was taken in nanoseconds.
* @hide
*/
@TestApi
public void setTimeOffsetNanos(double value) {
mTimeOffsetNanos = value;
}
/**
* Gets per-satellite sync state.
*
* <p>It represents the current sync state for the associated satellite.
*
* <p>This value helps interpret {@link #getReceivedSvTimeNanos()}.
*/
@State
public int getState() {
return mState;
}
/**
* Sets the sync state.
* @hide
*/
@TestApi
public void setState(@State int value) {
mState = value;
}
/**
* Gets a string representation of the 'sync state'.
*
* <p>For internal and logging use only.
*/
private String getStateString() {
if (mState == STATE_UNKNOWN) {
return "Unknown";
}
StringBuilder builder = new StringBuilder();
if ((mState & STATE_CODE_LOCK) != 0) {
builder.append("CodeLock|");
}
if ((mState & STATE_BIT_SYNC) != 0) {
builder.append("BitSync|");
}
if ((mState & STATE_SUBFRAME_SYNC) != 0) {
builder.append("SubframeSync|");
}
if ((mState & STATE_TOW_DECODED) != 0) {
builder.append("TowDecoded|");
}
if ((mState & STATE_TOW_KNOWN) != 0) {
builder.append("TowKnown|");
}
if ((mState & STATE_MSEC_AMBIGUOUS) != 0) {
builder.append("MsecAmbiguous|");
}
if ((mState & STATE_SYMBOL_SYNC) != 0) {
builder.append("SymbolSync|");
}
if ((mState & STATE_GLO_STRING_SYNC) != 0) {
builder.append("GloStringSync|");
}
if ((mState & STATE_GLO_TOD_DECODED) != 0) {
builder.append("GloTodDecoded|");
}
if ((mState & STATE_GLO_TOD_KNOWN) != 0) {
builder.append("GloTodKnown|");
}
if ((mState & STATE_BDS_D2_BIT_SYNC) != 0) {
builder.append("BdsD2BitSync|");
}
if ((mState & STATE_BDS_D2_SUBFRAME_SYNC) != 0) {
builder.append("BdsD2SubframeSync|");
}
if ((mState & STATE_GAL_E1BC_CODE_LOCK) != 0) {
builder.append("GalE1bcCodeLock|");
}
if ((mState & STATE_GAL_E1C_2ND_CODE_LOCK) != 0) {
builder.append("E1c2ndCodeLock|");
}
if ((mState & STATE_GAL_E1B_PAGE_SYNC) != 0) {
builder.append("GalE1bPageSync|");
}
if ((mState & STATE_SBAS_SYNC) != 0) {
builder.append("SbasSync|");
}
if ((mState & STATE_2ND_CODE_LOCK) != 0) {
builder.append("2ndCodeLock|");
}
int remainingStates = mState & ~STATE_ALL;
if (remainingStates > 0) {
builder.append("Other(");
builder.append(Integer.toBinaryString(remainingStates));
builder.append(")|");
}
builder.setLength(builder.length() - 1);
return builder.toString();
}
/**
* Gets the received GNSS satellite time, at the measurement time, in nanoseconds.
*
* <p>The received satellite time is relative to the beginning of the system week for all
* constellations except for Glonass where it is relative to the beginning of the Glonass
* system day.
*
* <p>The table below indicates the valid range of the received GNSS satellite time. These
* ranges depend on the constellation and code being tracked and the state of the tracking
* algorithms given by the {@link #getState} method. The minimum value of this field is zero.
* The maximum value of this field is determined by looking across all of the state flags
* that are set, for the given constellation and code type, and finding the the maximum value
* in this table.
*
* <p>For example, for GPS L1 C/A, if STATE_TOW_KNOWN is set, this field can be any value from 0
* to 1 week (in nanoseconds), and for GAL E1B code, if only STATE_GAL_E1BC_CODE_LOCK is set,
* then this field can be any value from 0 to 4 milliseconds (in nanoseconds.)
*
* <table border="1">
* <thead>
* <tr>
* <td />
* <td colspan="3"><strong>GPS/QZSS</strong></td>
* <td><strong>GLNS</strong></td>
* <td colspan="2"><strong>BDS</strong></td>
* <td colspan="3"><strong>GAL</strong></td>
* <td><strong>SBAS</strong></td>
* </tr>
* <tr>
* <td><strong>State Flag</strong></td>
* <td><strong>L1 C/A</strong></td>
* <td><strong>L5I</strong></td>
* <td><strong>L5Q</strong></td>
* <td><strong>L1OF</strong></td>
* <td><strong>B1I (D1)</strong></td>
* <td><strong>B1I &nbsp;(D2)</strong></td>
* <td><strong>E1B</strong></td>
* <td><strong>E1C</strong></td>
* <td><strong>E5AQ</strong></td>
* <td><strong>L1 C/A</strong></td>
* </tr>
* </thead>
* <tbody>
* <tr>
* <td>
* <strong>STATE_UNKNOWN</strong>
* </td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* <td>0</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_CODE_LOCK</strong>
* </td>
* <td>1 ms</td>
* <td>1 ms</td>
* <td>1 ms</td>
* <td>1 ms</td>
* <td>1 ms</td>
* <td>1 ms</td>
* <td>-</td>
* <td>-</td>
* <td>1 ms</td>
* <td>1 ms</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_SYMBOL_SYNC</strong>
* </td>
* <td>20 ms (optional)</td>
* <td>10 ms</td>
* <td>1 ms (optional)</td>
* <td>10 ms</td>
* <td>20 ms (optional)</td>
* <td>2 ms</td>
* <td>4 ms (optional)</td>
* <td>4 ms (optional)</td>
* <td>1 ms (optional)</td>
* <td>2 ms</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_BIT_SYNC</strong>
* </td>
* <td>20 ms</td>
* <td>20 ms</td>
* <td>1 ms (optional)</td>
* <td>20 ms</td>
* <td>20 ms</td>
* <td>-</td>
* <td>8 ms</td>
* <td>-</td>
* <td>1 ms (optional)</td>
* <td>4 ms</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_SUBFRAME_SYNC</strong>
* </td>
* <td>6s</td>
* <td>6s</td>
* <td>-</td>
* <td>2 s</td>
* <td>6 s</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>100 ms</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_TOW_DECODED</strong>
* </td>
* <td colspan="2">1 week</td>
* <td>-</td>
* <td>1 day</td>
* <td colspan="2">1 week</td>
* <td colspan="2">1 week</td>
* <td>-</td>
* <td>1 week</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_TOW_KNOWN</strong>
* </td>
* <td colspan="3">1 week</td>
* <td>1 day</td>
* <td colspan="2">1 week</td>
* <td colspan="3">1 week</td>
* <td>1 week</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_GLO_STRING_SYNC</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>2 s</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_GLO_TOD_DECODED</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>1 day</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_GLO_TOD_KNOWN</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>1 day</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_BDS_D2_BIT_SYNC</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>2 ms</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_BDS_D2_SUBFRAME_SYNC</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>600 ms</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_GAL_E1BC_CODE_LOCK</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>4 ms</td>
* <td>4 ms</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_GAL_E1C_2ND_CODE_LOCK</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>100 ms</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_2ND_CODE_LOCK</strong>
* </td>
* <td>-</td>
* <td>10 ms (optional)</td>
* <td>20 ms</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>100 ms (optional)</td>
* <td>100 ms</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_GAL_E1B_PAGE_SYNC</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>2 s</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* </tr>
* <tr>
* <td>
* <strong>STATE_SBAS_SYNC</strong>
* </td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>-</td>
* <td>1 s</td>
* </tr>
* </tbody>
* </table>
*
* <p>Note: TOW Known refers to the case where TOW is possibly not decoded over the air but has
* been determined from other sources. If TOW decoded is set then TOW Known must also be set.
*
* <p>Note well: if there is any ambiguity in integer millisecond, STATE_MSEC_AMBIGUOUS must be
* set accordingly, in the 'state' field. This value must be populated, unless the 'state' ==
* STATE_UNKNOWN.
*
* <p>Note on optional flags:
* <ul>
* <li> For L1 C/A and B1I, STATE_SYMBOL_SYNC is optional since the symbol length is the
* same as the bit length.
* <li> For L5Q and E5aQ, STATE_BIT_SYNC and STATE_SYMBOL_SYNC are optional since they are
* implied by STATE_CODE_LOCK.
* <li> STATE_2ND_CODE_LOCK for L5I is optional since it is implied by STATE_SYMBOL_SYNC.
* <li> STATE_2ND_CODE_LOCK for E1C is optional since it is implied by
* STATE_GAL_E1C_2ND_CODE_LOCK.
* <li> For E1B and E1C, STATE_SYMBOL_SYNC is optional, because it is implied by
* STATE_GAL_E1BC_CODE_LOCK.
* </ul>
*/
public long getReceivedSvTimeNanos() {
return mReceivedSvTimeNanos;
}
/**
* Sets the received GNSS time in nanoseconds.
* @hide
*/
@TestApi
public void setReceivedSvTimeNanos(long value) {
mReceivedSvTimeNanos = value;
}
/**
* Gets the error estimate (1-sigma) for the received GNSS time, in nanoseconds.
*/
public long getReceivedSvTimeUncertaintyNanos() {
return mReceivedSvTimeUncertaintyNanos;
}
/**
* Sets the received GNSS time uncertainty (1-Sigma) in nanoseconds.
* @hide
*/
@TestApi
public void setReceivedSvTimeUncertaintyNanos(long value) {
mReceivedSvTimeUncertaintyNanos = value;
}
/**
* Gets the Carrier-to-noise density in dB-Hz.
*
* <p>Typical range: 10-50 db-Hz.
*
* <p>The value contains the measured C/N0 for the signal at the antenna input.
*/
public double getCn0DbHz() {
return mCn0DbHz;
}
/**
* Sets the carrier-to-noise density in dB-Hz.
* @hide
*/
@TestApi
public void setCn0DbHz(double value) {
mCn0DbHz = value;
}
/**
* Returns {@code true} if {@link #getBasebandCn0DbHz()} is available, {@code false} otherwise.
*/
public boolean hasBasebandCn0DbHz() {
return isFlagSet(HAS_BASEBAND_CN0);
}
/**
* Gets the baseband carrier-to-noise density in dB-Hz.
*
* <p>Typical range: 0-50 dB-Hz.
*
* <p>The value contains the measured C/N0 for the signal at the baseband. This is typically
* a few dB weaker than the value estimated for C/N0 at the antenna port, which is reported
* in {@link #getCn0DbHz()}.
*/
@FloatRange(from = 0, to = 50)
public double getBasebandCn0DbHz() {
return mBasebandCn0DbHz;
}
/**
* Sets the baseband carrier-to-noise density in dB-Hz.
*
* @hide
*/
@TestApi
public void setBasebandCn0DbHz(double value) {
setFlag(HAS_BASEBAND_CN0);
mBasebandCn0DbHz = value;
}
/**
* Resets the baseband carrier-to-noise density in dB-Hz.
*
* @hide
*/
@TestApi
public void resetBasebandCn0DbHz() {
resetFlag(HAS_BASEBAND_CN0);
mBasebandCn0DbHz = Double.NaN;
}
/**
* Gets the Pseudorange rate at the timestamp in m/s.
*
* <p>The error estimate for this value is
* {@link #getPseudorangeRateUncertaintyMetersPerSecond()}.
*
* <p>The value is uncorrected, i.e. corrections for receiver and satellite clock frequency
* errors are not included.
*
* <p>A positive 'uncorrected' value indicates that the SV is moving away from the receiver. The
* sign of the 'uncorrected' 'pseudorange rate' and its relation to the sign of 'doppler shift'
* is given by the equation:
*
* <pre>
* pseudorange rate = -k * doppler shift (where k is a constant)</pre>
*/
public double getPseudorangeRateMetersPerSecond() {
return mPseudorangeRateMetersPerSecond;
}
/**
* Sets the pseudorange rate at the timestamp in m/s.
* @hide
*/
@TestApi
public void setPseudorangeRateMetersPerSecond(double value) {
mPseudorangeRateMetersPerSecond = value;
}
/**
* Gets the pseudorange's rate uncertainty (1-Sigma) in m/s.
*
* <p>The uncertainty is represented as an absolute (single sided) value.
*/
public double getPseudorangeRateUncertaintyMetersPerSecond() {
return mPseudorangeRateUncertaintyMetersPerSecond;
}
/**
* Sets the pseudorange's rate uncertainty (1-Sigma) in m/s.
* @hide
*/
@TestApi
public void setPseudorangeRateUncertaintyMetersPerSecond(double value) {
mPseudorangeRateUncertaintyMetersPerSecond = value;
}
/**
* Gets 'Accumulated Delta Range' state.
*
* <p>It indicates whether {@link #getAccumulatedDeltaRangeMeters()} is reset or there is a
* cycle slip (indicating 'loss of lock').
*/
@AdrState
public int getAccumulatedDeltaRangeState() {
return mAccumulatedDeltaRangeState;
}
/**
* Sets the 'Accumulated Delta Range' state.
* @hide
*/
@TestApi
public void setAccumulatedDeltaRangeState(@AdrState int value) {
mAccumulatedDeltaRangeState = value;
}
/**
* Gets a string representation of the 'Accumulated Delta Range state'.
*
* <p>For internal and logging use only.
*/
private String getAccumulatedDeltaRangeStateString() {
if (mAccumulatedDeltaRangeState == ADR_STATE_UNKNOWN) {
return "Unknown";
}
StringBuilder builder = new StringBuilder();
if ((mAccumulatedDeltaRangeState & ADR_STATE_VALID) == ADR_STATE_VALID) {
builder.append("Valid|");
}
if ((mAccumulatedDeltaRangeState & ADR_STATE_RESET) == ADR_STATE_RESET) {
builder.append("Reset|");
}
if ((mAccumulatedDeltaRangeState & ADR_STATE_CYCLE_SLIP) == ADR_STATE_CYCLE_SLIP) {
builder.append("CycleSlip|");
}
if ((mAccumulatedDeltaRangeState & ADR_STATE_HALF_CYCLE_RESOLVED) ==
ADR_STATE_HALF_CYCLE_RESOLVED) {
builder.append("HalfCycleResolved|");
}
if ((mAccumulatedDeltaRangeState & ADR_STATE_HALF_CYCLE_REPORTED)
== ADR_STATE_HALF_CYCLE_REPORTED) {
builder.append("HalfCycleReported|");
}
int remainingStates = mAccumulatedDeltaRangeState & ~ADR_STATE_ALL;
if (remainingStates > 0) {
builder.append("Other(");
builder.append(Integer.toBinaryString(remainingStates));
builder.append(")|");
}
builder.deleteCharAt(builder.length() - 1);
return builder.toString();
}
/**
* Gets the accumulated delta range since the last channel reset, in meters.
*
* <p>The error estimate for this value is {@link #getAccumulatedDeltaRangeUncertaintyMeters()}.
*
* <p>The availability of the value is represented by {@link #getAccumulatedDeltaRangeState()}.
*
* <p>A positive value indicates that the SV is moving away from the receiver.
* The sign of {@link #getAccumulatedDeltaRangeMeters()} and its relation to the sign of
* {@link #getCarrierPhase()} is given by the equation:
*
* <pre>
* accumulated delta range = -k * carrier phase (where k is a constant)</pre>
*
* <p>Similar to the concept of an RTCM "Phaserange", when the accumulated delta range is
* initially chosen, and whenever it is reset, it will retain the integer nature
* of the relative carrier phase offset between satellites observed by this receiver, such that
* the double difference of this value between receivers and satellites may be used, together
* with integer ambiguity resolution, to determine highly precise relative location between
* receivers.
*
* <p>This includes ensuring that all half-cycle ambiguities are resolved before this value is
* reported as {@link #ADR_STATE_VALID}.
*
* <p>The alignment of the phase measurement will not be adjusted by the receiver so the
* in-phase and quadrature phase components will have a quarter cycle offset as they do when
* transmitted from the satellites. If the measurement is from a combination of the in-phase
* and quadrature phase components, then the alignment of the phase measurement will be aligned
* to the in-phase component.
*/
public double getAccumulatedDeltaRangeMeters() {
return mAccumulatedDeltaRangeMeters;
}
/**
* Sets the accumulated delta range in meters.
* @hide
*/
@TestApi
public void setAccumulatedDeltaRangeMeters(double value) {
mAccumulatedDeltaRangeMeters = value;
}
/**
* Gets the accumulated delta range's uncertainty (1-Sigma) in meters.
*
* <p>The uncertainty is represented as an absolute (single sided) value.
*
* <p>The status of the value is represented by {@link #getAccumulatedDeltaRangeState()}.
*/
public double getAccumulatedDeltaRangeUncertaintyMeters() {
return mAccumulatedDeltaRangeUncertaintyMeters;
}
/**
* Sets the accumulated delta range's uncertainty (1-sigma) in meters.
*
* <p>The status of the value is represented by {@link #getAccumulatedDeltaRangeState()}.
*
* @hide
*/
@TestApi
public void setAccumulatedDeltaRangeUncertaintyMeters(double value) {
mAccumulatedDeltaRangeUncertaintyMeters = value;
}
/**
* Returns {@code true} if {@link #getCarrierFrequencyHz()} is available, {@code false}
* otherwise.
*/
public boolean hasCarrierFrequencyHz() {
return isFlagSet(HAS_CARRIER_FREQUENCY);
}
/**
* Gets the carrier frequency of the tracked signal.
*
* <p>For example it can be the GPS central frequency for L1 = 1575.45 MHz, or L2 = 1227.60 MHz,
* L5 = 1176.45 MHz, varying GLO channels, etc. If the field is not set, it is the primary
* common use central frequency, e.g. L1 = 1575.45 MHz for GPS.
*
* <p> For an L1, L5 receiver tracking a satellite on L1 and L5 at the same time, two raw
* measurement objects will be reported for this same satellite, in one of the measurement
* objects, all the values related to L1 will be filled, and in the other all of the values
* related to L5 will be filled.
*
* <p>The value is only available if {@link #hasCarrierFrequencyHz()} is {@code true}.
*
* @return the carrier frequency of the signal tracked in Hz.
*/
public float getCarrierFrequencyHz() {
return mCarrierFrequencyHz;
}
/**
* Sets the Carrier frequency in Hz.
* @hide
*/
@TestApi
public void setCarrierFrequencyHz(float carrierFrequencyHz) {
setFlag(HAS_CARRIER_FREQUENCY);
mCarrierFrequencyHz = carrierFrequencyHz;
}
/**
* Resets the Carrier frequency in Hz.
* @hide
*/
@TestApi
public void resetCarrierFrequencyHz() {
resetFlag(HAS_CARRIER_FREQUENCY);
mCarrierFrequencyHz = Float.NaN;
}
/**
* Returns {@code true} if {@link #getCarrierCycles()} is available, {@code false} otherwise.
*
* @deprecated use {@link #getAccumulatedDeltaRangeState()} instead.
*/
@Deprecated
public boolean hasCarrierCycles() {
return isFlagSet(HAS_CARRIER_CYCLES);
}
/**
* The number of full carrier cycles between the satellite and the receiver.
*
* <p>The reference frequency is given by the value of {@link #getCarrierFrequencyHz()}.
*
* <p>The value is only available if {@link #hasCarrierCycles()} is {@code true}.
*
* @deprecated use {@link #getAccumulatedDeltaRangeMeters()} instead.
*/
@Deprecated
public long getCarrierCycles() {
return mCarrierCycles;
}
/**
* Sets the number of full carrier cycles between the satellite and the receiver.
*
* @deprecated use {@link #setAccumulatedDeltaRangeMeters(double)}
* and {@link #setAccumulatedDeltaRangeState(int)} instead.
*
* @hide
*/
@TestApi
@Deprecated
public void setCarrierCycles(long value) {
setFlag(HAS_CARRIER_CYCLES);
mCarrierCycles = value;
}
/**
* Resets the number of full carrier cycles between the satellite and the receiver.
*
* @deprecated use {@link #setAccumulatedDeltaRangeMeters(double)}
* and {@link #setAccumulatedDeltaRangeState(int)} instead.
* @hide
*/
@TestApi
@Deprecated
public void resetCarrierCycles() {
resetFlag(HAS_CARRIER_CYCLES);
mCarrierCycles = Long.MIN_VALUE;
}
/**
* Returns {@code true} if {@link #getCarrierPhase()} is available, {@code false} otherwise.
*
* @deprecated use {@link #getAccumulatedDeltaRangeState()} instead.
*/
@Deprecated
public boolean hasCarrierPhase() {
return isFlagSet(HAS_CARRIER_PHASE);
}
/**
* Gets the RF phase detected by the receiver.
*
* <p>Range: [0.0, 1.0].
*
* <p>This is the fractional part of the complete carrier phase measurement.
*
* <p>The reference frequency is given by the value of {@link #getCarrierFrequencyHz()}.
*
* <p>The error estimate for this value is {@link #getCarrierPhaseUncertainty()}.
*
* <p>The value is only available if {@link #hasCarrierPhase()} is {@code true}.
*
* @deprecated use {@link #getAccumulatedDeltaRangeMeters()} instead.
*/
@Deprecated
public double getCarrierPhase() {
return mCarrierPhase;
}
/**
* Sets the RF phase detected by the receiver.
*
* @deprecated use {@link #setAccumulatedDeltaRangeMeters(double)}
* and {@link #setAccumulatedDeltaRangeState(int)} instead.
*
* @hide
*/
@TestApi
@Deprecated
public void setCarrierPhase(double value) {
setFlag(HAS_CARRIER_PHASE);
mCarrierPhase = value;
}
/**
* Resets the RF phase detected by the receiver.
*
* @deprecated use {@link #setAccumulatedDeltaRangeMeters(double)}
* and {@link #setAccumulatedDeltaRangeState(int)} instead.
*
* @hide
*/
@TestApi
@Deprecated
public void resetCarrierPhase() {
resetFlag(HAS_CARRIER_PHASE);
mCarrierPhase = Double.NaN;
}
/**
* Returns {@code true} if {@link #getCarrierPhaseUncertainty()} is available, {@code false}
* otherwise.
*
* @deprecated use {@link #getAccumulatedDeltaRangeState()} instead.
*/
@Deprecated
public boolean hasCarrierPhaseUncertainty() {
return isFlagSet(HAS_CARRIER_PHASE_UNCERTAINTY);
}
/**
* Gets the carrier-phase's uncertainty (1-Sigma).
*
* <p>The uncertainty is represented as an absolute (single sided) value.
*
* <p>The value is only available if {@link #hasCarrierPhaseUncertainty()} is {@code true}.
*
* @deprecated use {@link #getAccumulatedDeltaRangeUncertaintyMeters()} instead.
*/
@Deprecated
public double getCarrierPhaseUncertainty() {
return mCarrierPhaseUncertainty;
}
/**
* Sets the Carrier-phase's uncertainty (1-Sigma) in cycles.
*
* @deprecated use {@link #setAccumulatedDeltaRangeUncertaintyMeters(double)}
* and {@link #setAccumulatedDeltaRangeState(int)} instead.
*
* @hide
*/
@TestApi
@Deprecated
public void setCarrierPhaseUncertainty(double value) {
setFlag(HAS_CARRIER_PHASE_UNCERTAINTY);
mCarrierPhaseUncertainty = value;
}
/**
* Resets the Carrier-phase's uncertainty (1-Sigma) in cycles.
*
* @deprecated use {@link #setAccumulatedDeltaRangeUncertaintyMeters(double)}
* and {@link #setAccumulatedDeltaRangeState(int)} instead.
*
* @hide
*/
@TestApi
@Deprecated
public void resetCarrierPhaseUncertainty() {
resetFlag(HAS_CARRIER_PHASE_UNCERTAINTY);
mCarrierPhaseUncertainty = Double.NaN;
}
/**
* Gets a value indicating the 'multipath' state of the event.
*/
@MultipathIndicator
public int getMultipathIndicator() {
return mMultipathIndicator;
}
/**
* Sets the 'multi-path' indicator.
* @hide
*/
@TestApi
public void setMultipathIndicator(@MultipathIndicator int value) {
mMultipathIndicator = value;
}
/**
* Gets a string representation of the 'multi-path indicator'.
*
* <p>For internal and logging use only.
*/
private String getMultipathIndicatorString() {
switch (mMultipathIndicator) {
case MULTIPATH_INDICATOR_UNKNOWN:
return "Unknown";
case MULTIPATH_INDICATOR_DETECTED:
return "Detected";
case MULTIPATH_INDICATOR_NOT_DETECTED:
return "NotDetected";
default:
return "<Invalid: " + mMultipathIndicator + ">";
}
}
/**
* Returns {@code true} if {@link #getSnrInDb()} is available, {@code false} otherwise.
*/
public boolean hasSnrInDb() {
return isFlagSet(HAS_SNR);
}
/**
* Gets the (post-correlation & integration) Signal-to-Noise ratio (SNR) in dB.
*
* <p>The value is only available if {@link #hasSnrInDb()} is {@code true}.
*/
public double getSnrInDb() {
return mSnrInDb;
}
/**
* Sets the Signal-to-noise ratio (SNR) in dB.
* @hide
*/
@TestApi
public void setSnrInDb(double snrInDb) {
setFlag(HAS_SNR);
mSnrInDb = snrInDb;
}
/**
* Resets the Signal-to-noise ratio (SNR) in dB.
* @hide
*/
@TestApi
public void resetSnrInDb() {
resetFlag(HAS_SNR);
mSnrInDb = Double.NaN;
}
/**
* Returns {@code true} if {@link #getAutomaticGainControlLevelDb()} is available,
* {@code false} otherwise.
*/
public boolean hasAutomaticGainControlLevelDb() {
return isFlagSet(HAS_AUTOMATIC_GAIN_CONTROL);
}
/**
* Gets the Automatic Gain Control level in dB.
*
* <p> AGC acts as a variable gain amplifier adjusting the power of the incoming signal. The AGC
* level may be used to indicate potential interference. When AGC is at a nominal level, this
* value must be set as 0. Higher gain (and/or lower input power) shall be output as a positive
* number. Hence in cases of strong jamming, in the band of this signal, this value will go more
* negative.
*
* <p> Note: Different hardware designs (e.g. antenna, pre-amplification, or other RF HW
* components) may also affect the typical output of of this value on any given hardware design
* in an open sky test - the important aspect of this output is that changes in this value are
* indicative of changes on input signal power in the frequency band for this measurement.
*
* <p> The value is only available if {@link #hasAutomaticGainControlLevelDb()} is {@code true}
*/
public double getAutomaticGainControlLevelDb() {
return mAutomaticGainControlLevelInDb;
}
/**
* Sets the Automatic Gain Control level in dB.
* @hide
*/
@TestApi
public void setAutomaticGainControlLevelInDb(double agcLevelDb) {
setFlag(HAS_AUTOMATIC_GAIN_CONTROL);
mAutomaticGainControlLevelInDb = agcLevelDb;
}
/**
* Resets the Automatic Gain Control level.
* @hide
*/
@TestApi
public void resetAutomaticGainControlLevel() {
resetFlag(HAS_AUTOMATIC_GAIN_CONTROL);
mAutomaticGainControlLevelInDb = Double.NaN;
}
/**
* Returns {@code true} if {@link #getCodeType()} is available,
* {@code false} otherwise.
*/
public boolean hasCodeType() {
return isFlagSet(HAS_CODE_TYPE);
}
/**
* Gets the GNSS measurement's code type.
*
* <p>Similar to the Attribute field described in RINEX 3.03, e.g., in Tables 4-10, and Table
* A2 at the RINEX 3.03 Update 1 Document.
*
* <p>Returns "A" for GALILEO E1A, GALILEO E6A, IRNSS L5A, IRNSS SA.
*
* <p>Returns "B" for GALILEO E1B, GALILEO E6B, IRNSS L5B, IRNSS SB.
*
* <p>Returns "C" for GPS L1 C/A, GPS L2 C/A, GLONASS G1 C/A, GLONASS G2 C/A, GALILEO E1C,
* GALILEO E6C, SBAS L1 C/A, QZSS L1 C/A, IRNSS L5C.
*
* <p>Returns "I" for GPS L5 I, GLONASS G3 I, GALILEO E5a I, GALILEO E5b I, GALILEO E5a+b I,
* SBAS L5 I, QZSS L5 I, BDS B1 I, BDS B2 I, BDS B3 I.
*
* <p>Returns "L" for GPS L1C (P), GPS L2C (L), QZSS L1C (P), QZSS L2C (L), LEX(6) L.
*
* <p>Returns "M" for GPS L1M, GPS L2M.
*
* <p>Returns "N" for GPS L1 codeless, GPS L2 codeless.
*
* <p>Returns "P" for GPS L1P, GPS L2P, GLONASS G1P, GLONASS G2P.
*
* <p>Returns "Q" for GPS L5 Q, GLONASS G3 Q, GALILEO E5a Q, GALILEO E5b Q, GALILEO E5a+b Q,
* SBAS L5 Q, QZSS L5 Q, BDS B1 Q, BDS B2 Q, BDS B3 Q.
*
* <p>Returns "S" for GPS L1C (D), GPS L2C (M), QZSS L1C (D), QZSS L2C (M), LEX(6) S.
*
* <p>Returns "W" for GPS L1 Z-tracking, GPS L2 Z-tracking.
*
* <p>Returns "X" for GPS L1C (D+P), GPS L2C (M+L), GPS L5 (I+Q), GLONASS G3 (I+Q), GALILEO
* E1 (B+C), GALILEO E5a (I+Q), GALILEO E5b (I+Q), GALILEO E5a+b(I+Q), GALILEO E6 (B+C), SBAS
* L5 (I+Q), QZSS L1C (D+P), QZSS L2C (M+L), QZSS L5 (I+Q), LEX(6) (S+L), BDS B1 (I+Q), BDS
* B2 (I+Q), BDS B3 (I+Q), IRNSS L5 (B+C).
*
* <p>Returns "Y" for GPS L1Y, GPS L2Y.
*
* <p>Returns "Z" for GALILEO E1 (A+B+C), GALILEO E6 (A+B+C), QZSS L1-SAIF.
*
* <p>Returns "UNKNOWN" if the GNSS Measurement's code type is unknown.
*
* <p>This is used to specify the observation descriptor defined in GNSS Observation Data File
* Header Section Description in the RINEX standard (Version 3.XX), in cases where the code type
* does not align with the above listed values. For example, if a code type "G" is added, this
* string shall be set to "G".
*/
@NonNull
public String getCodeType() {
return mCodeType;
}
/**
* Sets the GNSS measurement's code type.
*
* @hide
*/
@TestApi
public void setCodeType(@NonNull String codeType) {
setFlag(HAS_CODE_TYPE);
mCodeType = codeType;
}
/**
* Resets the GNSS measurement's code type.
*
* @hide
*/
@TestApi
public void resetCodeType() {
resetFlag(HAS_CODE_TYPE);
mCodeType = "UNKNOWN";
}
public static final @android.annotation.NonNull Creator<GnssMeasurement> CREATOR = new Creator<GnssMeasurement>() {
@Override
public GnssMeasurement createFromParcel(Parcel parcel) {
GnssMeasurement gnssMeasurement = new GnssMeasurement();
gnssMeasurement.mFlags = parcel.readInt();
gnssMeasurement.mSvid = parcel.readInt();
gnssMeasurement.mConstellationType = parcel.readInt();
gnssMeasurement.mTimeOffsetNanos = parcel.readDouble();
gnssMeasurement.mState = parcel.readInt();
gnssMeasurement.mReceivedSvTimeNanos = parcel.readLong();
gnssMeasurement.mReceivedSvTimeUncertaintyNanos = parcel.readLong();
gnssMeasurement.mCn0DbHz = parcel.readDouble();
gnssMeasurement.mPseudorangeRateMetersPerSecond = parcel.readDouble();
gnssMeasurement.mPseudorangeRateUncertaintyMetersPerSecond = parcel.readDouble();
gnssMeasurement.mAccumulatedDeltaRangeState = parcel.readInt();
gnssMeasurement.mAccumulatedDeltaRangeMeters = parcel.readDouble();
gnssMeasurement.mAccumulatedDeltaRangeUncertaintyMeters = parcel.readDouble();
gnssMeasurement.mCarrierFrequencyHz = parcel.readFloat();
gnssMeasurement.mCarrierCycles = parcel.readLong();
gnssMeasurement.mCarrierPhase = parcel.readDouble();
gnssMeasurement.mCarrierPhaseUncertainty = parcel.readDouble();
gnssMeasurement.mMultipathIndicator = parcel.readInt();
gnssMeasurement.mSnrInDb = parcel.readDouble();
gnssMeasurement.mAutomaticGainControlLevelInDb = parcel.readDouble();
gnssMeasurement.mCodeType = parcel.readString();
gnssMeasurement.mBasebandCn0DbHz = parcel.readDouble();
return gnssMeasurement;
}
@Override
public GnssMeasurement[] newArray(int i) {
return new GnssMeasurement[i];
}
};
@Override
public void writeToParcel(Parcel parcel, int flags) {
parcel.writeInt(mFlags);
parcel.writeInt(mSvid);
parcel.writeInt(mConstellationType);
parcel.writeDouble(mTimeOffsetNanos);
parcel.writeInt(mState);
parcel.writeLong(mReceivedSvTimeNanos);
parcel.writeLong(mReceivedSvTimeUncertaintyNanos);
parcel.writeDouble(mCn0DbHz);
parcel.writeDouble(mPseudorangeRateMetersPerSecond);
parcel.writeDouble(mPseudorangeRateUncertaintyMetersPerSecond);
parcel.writeInt(mAccumulatedDeltaRangeState);
parcel.writeDouble(mAccumulatedDeltaRangeMeters);
parcel.writeDouble(mAccumulatedDeltaRangeUncertaintyMeters);
parcel.writeFloat(mCarrierFrequencyHz);
parcel.writeLong(mCarrierCycles);
parcel.writeDouble(mCarrierPhase);
parcel.writeDouble(mCarrierPhaseUncertainty);
parcel.writeInt(mMultipathIndicator);
parcel.writeDouble(mSnrInDb);
parcel.writeDouble(mAutomaticGainControlLevelInDb);
parcel.writeString(mCodeType);
parcel.writeDouble(mBasebandCn0DbHz);
}
@Override
public int describeContents() {
return 0;
}
@Override
public String toString() {
final String format = " %-29s = %s\n";
final String formatWithUncertainty = " %-29s = %-25s %-40s = %s\n";
StringBuilder builder = new StringBuilder("GnssMeasurement:\n");
builder.append(String.format(format, "Svid", mSvid));
builder.append(String.format(format, "ConstellationType", mConstellationType));
builder.append(String.format(format, "TimeOffsetNanos", mTimeOffsetNanos));
builder.append(String.format(format, "State", getStateString()));
builder.append(String.format(
formatWithUncertainty,
"ReceivedSvTimeNanos",
mReceivedSvTimeNanos,
"ReceivedSvTimeUncertaintyNanos",
mReceivedSvTimeUncertaintyNanos));
builder.append(String.format(format, "Cn0DbHz", mCn0DbHz));
builder.append(String.format(format, "BasebandCn0DbHz",
hasBasebandCn0DbHz() ? mBasebandCn0DbHz : null));
builder.append(String.format(
formatWithUncertainty,
"PseudorangeRateMetersPerSecond",
mPseudorangeRateMetersPerSecond,
"PseudorangeRateUncertaintyMetersPerSecond",
mPseudorangeRateUncertaintyMetersPerSecond));
builder.append(String.format(
format,
"AccumulatedDeltaRangeState",
getAccumulatedDeltaRangeStateString()));
builder.append(String.format(
formatWithUncertainty,
"AccumulatedDeltaRangeMeters",
mAccumulatedDeltaRangeMeters,
"AccumulatedDeltaRangeUncertaintyMeters",
mAccumulatedDeltaRangeUncertaintyMeters));
builder.append(String.format(
format,
"CarrierFrequencyHz",
hasCarrierFrequencyHz() ? mCarrierFrequencyHz : null));
builder.append(String.format(
format,
"CarrierCycles",
hasCarrierCycles() ? mCarrierCycles : null));
builder.append(String.format(
formatWithUncertainty,
"CarrierPhase",
hasCarrierPhase() ? mCarrierPhase : null,
"CarrierPhaseUncertainty",
hasCarrierPhaseUncertainty() ? mCarrierPhaseUncertainty : null));
builder.append(String.format(format, "MultipathIndicator", getMultipathIndicatorString()));
builder.append(String.format(
format,
"SnrInDb",
hasSnrInDb() ? mSnrInDb : null));
builder.append(String.format(
format,
"AgcLevelDb",
hasAutomaticGainControlLevelDb() ? mAutomaticGainControlLevelInDb : null));
builder.append(String.format(
format,
"CodeType",
hasCodeType() ? mCodeType : null));
return builder.toString();
}
private void initialize() {
mFlags = HAS_NO_FLAGS;
setSvid(0);
setTimeOffsetNanos(Long.MIN_VALUE);
setState(STATE_UNKNOWN);
setReceivedSvTimeNanos(Long.MIN_VALUE);
setReceivedSvTimeUncertaintyNanos(Long.MAX_VALUE);
setCn0DbHz(Double.MIN_VALUE);
setPseudorangeRateMetersPerSecond(Double.MIN_VALUE);
setPseudorangeRateUncertaintyMetersPerSecond(Double.MIN_VALUE);
setAccumulatedDeltaRangeState(ADR_STATE_UNKNOWN);
setAccumulatedDeltaRangeMeters(Double.MIN_VALUE);
setAccumulatedDeltaRangeUncertaintyMeters(Double.MIN_VALUE);
resetCarrierFrequencyHz();
resetCarrierCycles();
resetCarrierPhase();
resetCarrierPhaseUncertainty();
setMultipathIndicator(MULTIPATH_INDICATOR_UNKNOWN);
resetSnrInDb();
resetAutomaticGainControlLevel();
resetCodeType();
resetBasebandCn0DbHz();
}
private void setFlag(int flag) {
mFlags |= flag;
}
private void resetFlag(int flag) {
mFlags &= ~flag;
}
private boolean isFlagSet(int flag) {
return (mFlags & flag) == flag;
}
}