Files
pilotclient/tests/blackmisc/testinterpolatorparts.cpp
Klaus Basan 0808cdb223 Ref T261, further unify interpolator handling
* return interpolation results parts/situation in one step
* base class init for each interpolation step, less redundant code
* removed old interpolation/parts function
* adjusted unit tests and simulator objects (such as SimObject)
2018-05-08 16:06:52 +02:00

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6.7 KiB
C++

/* Copyright (C) 2018
* swift project Community / Contributors
*
* This file is part of swift project. It is subject to the license terms in the LICENSE file found in the top-level
* directory of this distribution and at http://www.swift-project.org/license.html. No part of swift project,
* including this file, may be copied, modified, propagated, or distributed except according to the terms
* contained in the LICENSE file.
*/
//! \cond PRIVATE_TESTS
/*!
* \file
* \ingroup testblackmisc
*/
#include "testinterpolatorparts.h"
#include "blackmisc/simulation/interpolatorspline.h"
#include "blackmisc/simulation/remoteaircraftproviderdummy.h"
#include <QTest>
#include <QtDebug>
using namespace BlackMisc;
using namespace BlackMisc::Aviation;
using namespace BlackMisc::Geo;
using namespace BlackMisc::PhysicalQuantities;
using namespace BlackMisc::Simulation;
namespace BlackMiscTest
{
void CTestInterpolatorParts::groundFlagInterpolation()
{
CCallsign cs("SWIFT");
CRemoteAircraftProviderDummy provider;
CInterpolatorSpline interpolator(cs, nullptr, nullptr, &provider);
// fixed time so everything can be debugged
const qint64 ts = 1425000000000; // QDateTime::currentMSecsSinceEpoch()
const qint64 deltaT = 5000; // ms
const int number = CRemoteAircraftProviderDummy::MaxPartsPerCallsign;
// const int numberHalf = number / 2;
const qint64 farFuture = ts + 3 * number * deltaT;
const qint64 farPast = ts - 4 * number * deltaT;
CAircraftPartsList parts;
for (int i = 0; i < number; i++)
{
const CAircraftParts p = createTestParts(i, ts, deltaT, true);
parts.push_back(p);
}
QVERIFY2(parts.size() == number, "Wrong parts size of list");
// interpolation functional check
const CInterpolationAndRenderingSetupPerCallsign setup;
const qint64 oldestTs = parts.oldestTimestampMsecsSinceEpoch();
// Testing for a time >> last time
// all on ground flags true
provider.insertNewAircraftParts(cs, parts, false); // we work with 0 offsets here
QVERIFY2(provider.remoteAircraftPartsCount(cs) == parts.size(), "Wrong parts size");
CInterpolationResult result = interpolator.getInterpolation(farFuture, setup);
CAircraftParts p = result;
qint64 pTs = p.getAdjustedMSecsSinceEpoch();
QVERIFY2(result.getPartsStatus().isSupportingParts(), "Should support parts");
QVERIFY2(pTs == ts, "Expect latest ts");
result = interpolator.getInterpolation(farPast, setup);
p = result;
pTs = p.getAdjustedMSecsSinceEpoch();
QVERIFY2(result.getPartsStatus().isSupportingParts(), "Should support parts");
QVERIFY2(pTs == oldestTs, "Expect oldest ts");
// Testing for a time >> last time
// all on ground flags true
interpolator.clear();
provider.clear();
parts.setOnGround(false);
provider.insertNewAircraftParts(cs, parts, false); // we work with 0 offsets here
result = interpolator.getInterpolation(farFuture, setup);
p = result;
pTs = p.getAdjustedMSecsSinceEpoch();
QVERIFY2(result.getPartsStatus().isSupportingParts(), "Should support parts");
QVERIFY2(p.getAdjustedMSecsSinceEpoch() == pTs, "Expect latest ts");
}
void CTestInterpolatorParts::partsToSituationGndFlag()
{
CCallsign cs("SWIFT");
// fixed time so everything can be debugged
const qint64 ts = 1425000000000; // QDateTime::currentMSecsSinceEpoch()
const qint64 deltaT = 5000; // ms
const int number = 10;
CAircraftPartsList partsOnGround;
for (int i = 0; i < number; i++)
{
const CAircraftParts p = createTestParts(i, ts, deltaT, true);
partsOnGround.push_back(p);
}
CAircraftPartsList partsNotOnGround;
for (int i = 0; i < number; i++)
{
const CAircraftParts p = createTestParts(i, ts, deltaT, false);
partsNotOnGround.push_back(p);
}
CAircraftSituationList situations;
for (int i = 0; i < number; i++)
{
CAircraftSituation s = createTestSituation(cs, i, ts, deltaT, 0);
s.setOnGround(CAircraftSituation::OnGroundSituationUnknown, CAircraftSituation::NotSetGroundDetails);
situations.push_back(s);
}
CAircraftSituation s0 = situations[0];
s0.adjustGroundFlag(partsOnGround, true);
QVERIFY2(s0.getOnGround(), "Supposed to be on ground");
s0 = situations[0];
s0.adjustGroundFlag(partsNotOnGround, true);
QVERIFY2(!s0.getOnGround(), "Supposed to be not on ground");
qint64 distanceMs = -1;
const qint64 Offset = 33;
partsOnGround.addMsecsToOffset(Offset);
CAircraftSituation s1 = situations[1];
s1.setOnGroundDetails(CAircraftSituation::NotSetGroundDetails);
s1.adjustGroundFlag(partsOnGround, true, 0.1, &distanceMs);
QVERIFY2(s1.getOnGround(), "Supposed to be on ground");
QVERIFY2(distanceMs == deltaT - Offset, "Offset time wrong");
QVERIFY2(s1.getOnGroundDetails() == CAircraftSituation::InFromParts, "Wrong details");
}
CAircraftParts CTestInterpolatorParts::createTestParts(int number, qint64 ts, qint64 deltaT, bool onGround)
{
CAircraftLights l(true, false, true, false, true, false);
CAircraftEngineList e({ CAircraftEngine(1, true), CAircraftEngine(2, false), CAircraftEngine(3, true) });
CAircraftParts p(l, true, 20, true, e, false);
p.setMSecsSinceEpoch(ts - deltaT * number); // values in past
p.setTimeOffsetMs(0);
p.setOnGround(onGround);
return p;
}
CAircraftSituation CTestInterpolatorParts::createTestSituation(const CCallsign &callsign, int number, qint64 ts, qint64 deltaT, qint64 offset)
{
const CAltitude alt(number, CAltitude::MeanSeaLevel, CLengthUnit::m());
const CLatitude lat(number, CAngleUnit::deg());
const CLongitude lng(180.0 + number, CAngleUnit::deg());
const CHeading heading(number * 10, CHeading::True, CAngleUnit::deg());
const CAngle bank(number, CAngleUnit::deg());
const CAngle pitch(number, CAngleUnit::deg());
const CSpeed gs(number * 10, CSpeedUnit::km_h());
const CAltitude gndElev({ 0, CLengthUnit::m() }, CAltitude::MeanSeaLevel);
const CCoordinateGeodetic c(lat, lng, alt);
CAircraftSituation s(callsign, c, heading, pitch, bank, gs);
s.setGroundElevation(gndElev);
s.setMSecsSinceEpoch(ts - deltaT * number); // values in past
s.setTimeOffsetMs(offset);
return s;
}
} // namespace
//! \endcond