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* no longer needed with providers in that form * pure refactoring commit, just guarantees compilation * already minor adjustments to use providers
192 lines
9.9 KiB
C++
192 lines
9.9 KiB
C++
/* Copyright (C) 2014
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* swift project Community / Contributors
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*
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* This file is part of swift project. It is subject to the license terms in the LICENSE file found in the top-level
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* directory of this distribution and at http://www.swift-project.org/license.html. No part of swift project,
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* including this file, may be copied, modified, propagated, or distributed except according to the terms
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* contained in the LICENSE file.
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*/
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#include "interpolatorlinear.h"
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#include "blackmisc/aviation/aircraftsituation.h"
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#include "blackmisc/aviation/aircraftsituationlist.h"
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#include "blackmisc/aviation/altitude.h"
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#include "blackmisc/geo/coordinategeodetic.h"
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#include "blackmisc/pq/length.h"
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#include "blackmisc/pq/physicalquantity.h"
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#include "blackmisc/logmessage.h"
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#include "blackmisc/compare.h"
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#include "blackmisc/verify.h"
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#include "blackmisc/range.h"
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#include "blackmisc/sequence.h"
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#include "blackmisc/statusmessage.h"
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#include <QDateTime>
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#include <QList>
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#include <array>
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using namespace BlackMisc::Aviation;
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using namespace BlackMisc::Geo;
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using namespace BlackMisc::Math;
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using namespace BlackMisc::PhysicalQuantities;
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using namespace BlackMisc::Simulation;
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namespace BlackMisc
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{
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namespace Simulation
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{
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CInterpolatorLinear::Interpolant::Interpolant(const CAircraftSituation &situation) :
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m_situationsAvailable(1), m_oldSituation(situation),
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m_pbh(0, situation, situation)
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{}
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CInterpolatorLinear::Interpolant::Interpolant(const CAircraftSituation &situation1, const CAircraftSituation &situation2, double timeFraction, qint64 interpolatedTime) :
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m_situationsAvailable(2),
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m_oldSituation(situation1), m_newSituation(situation2),
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m_simulationTimeFraction(timeFraction),
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m_interpolatedTime(interpolatedTime),
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m_pbh(m_simulationTimeFraction, situation1, situation2)
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{}
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CInterpolatorLinear::Interpolant CInterpolatorLinear::getInterpolant(
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qint64 currentTimeMsSinceEpoc,
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const CInterpolationAndRenderingSetupPerCallsign &setup,
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CInterpolationStatus &status, SituationLog &log) const
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{
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Q_UNUSED(setup);
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status.reset();
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// with the latest updates of T243 the order and the offsets are supposed to be correct
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// so even mixing fast/slow updates shall work
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BLACK_VERIFY_X(m_aircraftSituations.isSortedAdjustedLatestFirst(), Q_FUNC_INFO, "Wrong sort order");
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Q_ASSERT_X(m_aircraftSituations.size() <= IRemoteAircraftProvider::MaxSituationsPerCallsign, Q_FUNC_INFO, "Wrong size");
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// Ref T243, KB 2018-02, can be removed in future, we verify situations above
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// Situations are supposed to be in correct order
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// const auto end = std::is_sorted_until(m_aircraftSituations.begin(), m_aircraftSituations.end(), [](auto && a, auto && b) { return b.getAdjustedMSecsSinceEpoch() < a.getAdjustedMSecsSinceEpoch(); });
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// const auto validSituations = makeRange(m_aircraftSituations.begin(), end);
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// find the first situation earlier than the current time
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const CAircraftSituationList &validSituations = m_aircraftSituations; // if needed, we could also copy here
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const auto pivot = std::partition_point(validSituations.begin(), validSituations.end(), [ = ](auto &&s) { return s.getAdjustedMSecsSinceEpoch() > currentTimeMsSinceEpoc; });
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const auto situationsNewer = makeRange(validSituations.begin(), pivot);
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const auto situationsOlder = makeRange(pivot, validSituations.end());
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// interpolation situations
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CAircraftSituation oldSituation;
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CAircraftSituation newSituation;
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// latest first, now 00:20 split time
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// time pos
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// 00:25 10 newer
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// 00:20 11 newer
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// <----- split
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// 00:15 12 older
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// 00:10 13 older
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// 00:05 14 older
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// The first condition covers a situation, when there are no before / after situations.
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// We just place at the last position until we get before / after situations
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if (situationsOlder.isEmpty() || situationsNewer.isEmpty())
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{
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// no before situations
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if (situationsOlder.isEmpty())
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{
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const CAircraftSituation currentSituation(*(situationsNewer.end() - 1)); // oldest newest
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status.setInterpolatedAndCheckSituation(false, currentSituation);
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return currentSituation;
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}
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// only one before situation
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if (situationsOlder.size() < 2)
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{
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const CAircraftSituation currentSituation(situationsOlder.front()); // latest oldest
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status.setInterpolatedAndCheckSituation(false, currentSituation);
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return currentSituation;
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}
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// extrapolate from two before situations
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oldSituation = *(situationsOlder.begin() + 1); // before newest
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newSituation = situationsOlder.front(); // newest
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}
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else
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{
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oldSituation = situationsOlder.front(); // first oldest (aka newest oldest)
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newSituation = *(situationsNewer.end() - 1); // latest newest (aka oldest of newer block)
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Q_ASSERT(oldSituation.getAdjustedMSecsSinceEpoch() < newSituation.getAdjustedMSecsSinceEpoch());
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}
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// take hint into account to calculate elevation and above ground level
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// do not call for XP (lazy init)
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const CElevationPlane planeOld = this->findClosestElevationWithinRange(oldSituation, CElevationPlane::singlePointRadius());
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const CElevationPlane planeNew = this->findClosestElevationWithinRange(newSituation, CElevationPlane::singlePointRadius());
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oldSituation.setGroundElevationChecked(planeOld);
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newSituation.setGroundElevationChecked(planeNew);
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CAircraftSituation currentSituation(oldSituation); // also sets ground elevation if available
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// Time between start and end packet
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const double sampleDeltaTimeMs = newSituation.getAdjustedMSecsSinceEpoch() - oldSituation.getAdjustedMSecsSinceEpoch();
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Q_ASSERT_X(sampleDeltaTimeMs >= 0, Q_FUNC_INFO, "Negative delta time");
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log.interpolator = 'l';
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// Fraction of the deltaTime, ideally [0.0 - 1.0]
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// < 0 should not happen due to the split, > 1 can happen if new values are delayed beyond split time
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// 1) values > 1 mean extrapolation
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// 2) values > 2 mean no new situations coming in
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const double distanceToSplitTimeMs = newSituation.getAdjustedMSecsSinceEpoch() - currentTimeMsSinceEpoc;
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const double simulationTimeFraction = qMax(1.0 - (distanceToSplitTimeMs / sampleDeltaTimeMs), 0.0);
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const double deltaTimeFractionMs = sampleDeltaTimeMs * simulationTimeFraction;
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const qint64 interpolatedTime = oldSituation.getMSecsSinceEpoch() + deltaTimeFractionMs;
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currentSituation.setTimeOffsetMs(oldSituation.getTimeOffsetMs() + (newSituation.getTimeOffsetMs() - oldSituation.getTimeOffsetMs()) * simulationTimeFraction);
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currentSituation.setMSecsSinceEpoch(interpolatedTime);
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status.setInterpolatedAndCheckSituation(true, currentSituation);
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if (this->hasAttachedLogger() && setup.logInterpolation())
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{
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log.tsCurrent = currentTimeMsSinceEpoc;
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log.deltaSampleTimesMs = sampleDeltaTimeMs;
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log.simulationTimeFraction = simulationTimeFraction;
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log.deltaSampleTimesMs = sampleDeltaTimeMs;
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log.tsInterpolated = interpolatedTime;
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log.interpolationSituations.clear();
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log.interpolationSituations.push_back(newSituation); // newest at front
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log.interpolationSituations.push_back(oldSituation); // oldest at back
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}
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return { oldSituation, newSituation, simulationTimeFraction, interpolatedTime };
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}
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CCoordinateGeodetic CInterpolatorLinear::Interpolant::interpolatePosition(const CInterpolationAndRenderingSetupPerCallsign &setup) const
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{
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Q_UNUSED(setup);
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const std::array<double, 3> oldVec(m_oldSituation.getPosition().normalVectorDouble());
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const std::array<double, 3> newVec(m_newSituation.getPosition().normalVectorDouble());
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// Interpolate position: pos = (posB - posA) * t + posA
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CCoordinateGeodetic currentPosition;
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currentPosition.setNormalVector((newVec[0] - oldVec[0]) * m_simulationTimeFraction + oldVec[0],
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(newVec[1] - oldVec[1]) * m_simulationTimeFraction + oldVec[1],
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(newVec[2] - oldVec[2]) * m_simulationTimeFraction + oldVec[2]);
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return currentPosition;
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}
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CAltitude CInterpolatorLinear::Interpolant::interpolateAltitude(const CInterpolationAndRenderingSetupPerCallsign &setup) const
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{
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Q_UNUSED(setup);
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// Interpolate altitude: Alt = (AltB - AltA) * t + AltA
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// avoid underflow below ground elevation by using getCorrectedAltitude
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const CAltitude oldAlt(m_oldSituation.getCorrectedAltitude());
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const CAltitude newAlt(m_newSituation.getCorrectedAltitude());
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Q_ASSERT_X(oldAlt.getReferenceDatum() == CAltitude::MeanSeaLevel && oldAlt.getReferenceDatum() == newAlt.getReferenceDatum(), Q_FUNC_INFO, "mismatch in reference"); // otherwise no calculation is possible
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return CAltitude((newAlt - oldAlt)
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* m_simulationTimeFraction
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+ oldAlt,
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oldAlt.getReferenceDatum());
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}
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} // namespace
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} // namespace
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