/* * Copyright (C) 2019 James Turner * * This file is part of the program FlightGear. * * This program is free software: you can redistribute it and/or modify * it under the terms of the GNU General Public License as published by * the Free Software Foundation, either version 2 of the License, or * (at your option) any later version. * * This program is distributed in the hope that it will be useful, * but WITHOUT ANY WARRANTY; without even the implied warranty of * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the * GNU General Public License for more details. * * You should have received a copy of the GNU General Public License * along with this program. If not, see . */ #include "test_rnav_procedures.hxx" #include #include #include "test_suite/FGTestApi/testGlobals.hxx" #include "test_suite/FGTestApi/NavDataCache.hxx" #include "test_suite/FGTestApi/TestPilot.hxx" #include #include #include #include #include #include #include #include using namespace flightgear; ///////////////////////////////////////////////////////////////////////////// namespace { class TestFPDelegate : public FlightPlan::Delegate { public: FlightPlanRef thePlan; int sequenceCount = 0; virtual ~TestFPDelegate() { } void sequence() override { ++sequenceCount; int newIndex = thePlan->currentIndex() + 1; if (newIndex >= thePlan->numLegs()) { thePlan->finish(); return; } thePlan->setCurrentIndex(newIndex); } void currentWaypointChanged() override { } void departureChanged() override { // mimic the default delegate, inserting the SID waypoints // clear anything existing thePlan->clearWayptsWithFlag(WPT_DEPARTURE); // insert waypt for the dpearture runway auto dr = new RunwayWaypt(thePlan->departureRunway(), thePlan); dr->setFlag(WPT_DEPARTURE); thePlan->insertWayptAtIndex(dr, 0); if (thePlan->sid()) { WayptVec sidRoute; bool ok = thePlan->sid()->route(thePlan->departureRunway(), nullptr, sidRoute); if (!ok) throw sg_exception("failed to route via SID"); int insertIndex = 1; for (auto w : sidRoute) { thePlan->insertWayptAtIndex(w, insertIndex++); } } } }; } // of anonymous namespace ///////////////////////////////////////////////////////////////////////////// // Set up function for each test. void RNAVProcedureTests::setUp() { FGTestApi::setUp::initTestGlobals("rnav-procedures"); FGTestApi::setUp::initNavDataCache(); SGPath proceduresPath = SGPath::fromEnv("FG_PROCEDURES_PATH"); if (proceduresPath.exists()) { globals->append_fg_scenery(proceduresPath); } setupRouteManager(); } // Clean up after each test. void RNAVProcedureTests::tearDown() { FGTestApi::tearDown::shutdownTestGlobals(); } GPS* RNAVProcedureTests::setupStandardGPS(SGPropertyNode_ptr config, const std::string name, const int index) { SGPropertyNode_ptr configNode(config.valid() ? config : SGPropertyNode_ptr{new SGPropertyNode}); configNode->setStringValue("name", name); configNode->setIntValue("number", index); GPS* gps(new GPS(configNode)); m_gps = gps; m_gpsNode = globals->get_props()->getNode("instrumentation", true)->getChild(name, index, true); m_gpsNode->setBoolValue("serviceable", true); globals->get_props()->setDoubleValue("systems/electrical/outputs/gps", 6.0); gps->bind(); gps->init(); globals->add_subsystem("gps", gps, SGSubsystemMgr::POST_FDM); return gps; } void RNAVProcedureTests::setupRouteManager() { auto rm = globals->add_new_subsystem(); rm->bind(); rm->init(); rm->postinit(); } void RNAVProcedureTests::setPositionAndStabilise(const SGGeod& g) { FGTestApi::setPosition(g); for (int i=0; i<60; ++i) { m_gps->update(0.015); } } ///////////////////////////////////////////////////////////////////////////// #if 0 void RNAVProcedureTests::testBasic() { setupStandardGPS(); FGPositioned::TypeFilter f{FGPositioned::VOR}; auto bodrumVOR = fgpositioned_cast(FGPositioned::findClosestWithIdent("BDR", SGGeod::fromDeg(27.6, 37), &f)); SGGeod p1 = SGGeodesy::direct(bodrumVOR->geod(), 45.0, 5.0 * SG_NM_TO_METER); FGTestApi::setPositionAndStabilise(p1); } #endif void RNAVProcedureTests::testHeadingToAlt() { auto vhhh = FGAirport::findByIdent("VHHH"); FGTestApi::setUp::logPositionToKML("heading_to_alt"); auto rm = globals->get_subsystem(); auto fp = new FlightPlan; auto testDelegate = new TestFPDelegate; testDelegate->thePlan = fp; fp->addDelegate(testDelegate); rm->setFlightPlan(fp); // we don't have Nasal, but our delegate does the same work FGTestApi::setUp::populateFPWithNasal(fp, "VHHH", "25R", "EGLL", "27R", "HAZEL"); auto wp = new HeadingToAltitude(fp, "TO_4000", 270); wp->setAltitude(4000, RESTRICT_ABOVE); fp->insertWayptAtIndex(wp, 1); // between the runway WP and HAZEL FGTestApi::writeFlightPlanToKML(fp); auto depRwy = fp->departureRunway(); setupStandardGPS(); setPositionAndStabilise(fp->departureRunway()->pointOnCenterline(0.0)); fp->activate(); m_gpsNode->setStringValue("command", "leg"); CPPUNIT_ASSERT_EQUAL(fp->currentIndex(), 0); auto pilot = SGSharedPtr(new FGTestApi::TestPilot); pilot->resetAtPosition(depRwy->pointOnCenterline(0.0)); pilot->setCourseTrue(depRwy->headingDeg()); pilot->setSpeedKts(200); pilot->flyGPSCourse(m_gps); // check we sequence to the heading-to-alt wp bool ok = FGTestApi::runForTimeWithCheck(240.0, [fp] () { if (fp->currentIndex() == 1) { return true; } return false; }); CPPUNIT_ASSERT(ok); // leisurely climb out pilot->setVerticalFPM(1800); pilot->setTargetAltitudeFtMSL(8000); CPPUNIT_ASSERT_EQUAL(std::string{"VHHH-25R"}, std::string{m_gpsNode->getStringValue("wp/wp[0]/ID")}); CPPUNIT_ASSERT_EQUAL(std::string{"TO_4000"}, std::string{m_gpsNode->getStringValue("wp/wp[1]/ID")}); CPPUNIT_ASSERT_DOUBLES_EQUAL(270.0, m_gpsNode->getDoubleValue("wp/wp[1]/bearing-true-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(270.0, m_gpsNode->getDoubleValue("wp/leg-true-course-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-deviation-deg"), 0.5); // fly until we're turned to to heading ok = FGTestApi::runForTimeWithCheck(20, [pilot] () { return pilot->isOnHeading(270.); }); CPPUNIT_ASSERT(ok); // capture the position now SGGeod posAtHdgAltStart = globals->get_aircraft_position(); FGTestApi::runForTime(40.0); CPPUNIT_ASSERT_DOUBLES_EQUAL(270.0, m_gpsNode->getDoubleValue("wp/wp[1]/bearing-true-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(270.0, m_gpsNode->getDoubleValue("wp/leg-true-course-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-deviation-deg"), 0.5); const double crs = SGGeodesy::courseDeg(posAtHdgAltStart, globals->get_aircraft_position()); CPPUNIT_ASSERT_DOUBLES_EQUAL(270.0, crs, 1.0); ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { return (fp->currentIndex() == 2); }); CPPUNIT_ASSERT(ok); CPPUNIT_ASSERT_DOUBLES_EQUAL(4000.0, globals->get_aircraft_position().getElevationFt(), 100.0); FGTestApi::runForTime(40.0); } // ugly version: the heading to hold will be very mis-aligned with // the course when the leg is sequenced. (more than 90 degrees turn( void RNAVProcedureTests::testUglyHeadingToAlt() { auto vhhh = FGAirport::findByIdent("VHHH"); FGTestApi::setUp::logPositionToKML("heading_to_alt_ugly"); auto rm = globals->get_subsystem(); auto fp = new FlightPlan; auto testDelegate = new TestFPDelegate; testDelegate->thePlan = fp; fp->addDelegate(testDelegate); rm->setFlightPlan(fp); // we don't have Nasal, but our delegate does the same work FGTestApi::setUp::populateFPWithNasal(fp, "VHHH", "07L", "EGLL", "27R", "HAZEL"); auto wp = new HeadingToAltitude(fp, "TO_4000", 210); wp->setAltitude(4000, RESTRICT_ABOVE); fp->insertWayptAtIndex(wp, 1); // between the runway WP and HAZEL FGTestApi::writeFlightPlanToKML(fp); auto depRwy = fp->departureRunway(); setupStandardGPS(); setPositionAndStabilise(fp->departureRunway()->pointOnCenterline(0.0)); fp->activate(); m_gpsNode->setStringValue("command", "leg"); CPPUNIT_ASSERT_EQUAL(fp->currentIndex(), 0); auto pilot = SGSharedPtr(new FGTestApi::TestPilot); pilot->resetAtPosition(depRwy->pointOnCenterline(0.0)); pilot->setCourseTrue(depRwy->headingDeg()); pilot->setSpeedKts(200); pilot->flyGPSCourse(m_gps); // check we sequence to the heading-to-alt wp bool ok = FGTestApi::runForTimeWithCheck(240.0, [fp] () { if (fp->currentIndex() == 1) { return true; } return false; }); CPPUNIT_ASSERT(ok); // leisurely climb out pilot->setVerticalFPM(1800); pilot->setTargetAltitudeFtMSL(8000); CPPUNIT_ASSERT_EQUAL(std::string{"VHHH-07L"}, std::string{m_gpsNode->getStringValue("wp/wp[0]/ID")}); CPPUNIT_ASSERT_EQUAL(std::string{"TO_4000"}, std::string{m_gpsNode->getStringValue("wp/wp[1]/ID")}); CPPUNIT_ASSERT_DOUBLES_EQUAL(210.0, m_gpsNode->getDoubleValue("wp/wp[1]/bearing-true-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(210.0, m_gpsNode->getDoubleValue("wp/leg-true-course-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-deviation-deg"), 0.5); // fly until we're turned to to heading ok = FGTestApi::runForTimeWithCheck(120, [pilot] () { return pilot->isOnHeading(210.0); }); CPPUNIT_ASSERT(ok); // capture the position now SGGeod posAtHdgAltStart = globals->get_aircraft_position(); FGTestApi::runForTime(40.0); CPPUNIT_ASSERT_DOUBLES_EQUAL(210.0, m_gpsNode->getDoubleValue("wp/wp[1]/bearing-true-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(210.0, m_gpsNode->getDoubleValue("wp/leg-true-course-deg"), 0.5); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-deviation-deg"), 0.5); const double crs = SGGeodesy::courseDeg(posAtHdgAltStart, globals->get_aircraft_position()); CPPUNIT_ASSERT_DOUBLES_EQUAL(210.0, crs, 1.0); ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { return (fp->currentIndex() == 2); }); CPPUNIT_ASSERT(ok); CPPUNIT_ASSERT_DOUBLES_EQUAL(4000.0, globals->get_aircraft_position().getElevationFt(), 100.0); FGTestApi::runForTime(40.0); } void RNAVProcedureTests::testEGPH_TLA6C() { auto egph = FGAirport::findByIdent("EGPH"); auto sid = egph->findSIDWithIdent("TLA6C"); // procedures not loaded, abandon test if (!sid) return; FGTestApi::setUp::logPositionToKML("procedure_egph_tla6c"); auto rm = globals->get_subsystem(); auto fp = new FlightPlan; auto testDelegate = new TestFPDelegate; testDelegate->thePlan = fp; fp->addDelegate(testDelegate); rm->setFlightPlan(fp); FGTestApi::setUp::populateFPWithNasal(fp, "EGPH", "24", "EGLL", "27R", "DCS POL DTY"); fp->setSID(sid); FGRunwayRef departureRunway = fp->departureRunway(); CPPUNIT_ASSERT_EQUAL(std::string{"24"}, fp->legAtIndex(0)->waypoint()->source()->name()); CPPUNIT_ASSERT_EQUAL(std::string{"UW"}, fp->legAtIndex(1)->waypoint()->ident()); auto d242Wpt = fp->legAtIndex(2)->waypoint(); CPPUNIT_ASSERT_EQUAL(std::string{"D242H"}, d242Wpt->ident()); CPPUNIT_ASSERT_EQUAL(true, d242Wpt->flag(WPT_OVERFLIGHT)); CPPUNIT_ASSERT_EQUAL(std::string{"D346T"}, fp->legAtIndex(3)->waypoint()->ident()); FGTestApi::writeFlightPlanToKML(fp); CPPUNIT_ASSERT(rm->activate()); setupStandardGPS(); FGTestApi::setPositionAndStabilise(departureRunway->threshold()); m_gpsNode->setStringValue("command", "leg"); auto pilot = SGSharedPtr(new FGTestApi::TestPilot); pilot->resetAtPosition(globals->get_aircraft_position()); CPPUNIT_ASSERT_DOUBLES_EQUAL(departureRunway->headingDeg(), m_gpsNode->getDoubleValue("wp/leg-true-course-deg"), 0.5); pilot->setCourseTrue(m_gpsNode->getDoubleValue("wp/leg-true-course-deg")); pilot->setSpeedKts(220); pilot->flyGPSCourse(m_gps); FGTestApi::runForTime(20.0); // check we're somewhere along the runway, on the centerline // and still on waypoint zero bool ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { if (fp->currentIndex() == 1) { return true; } return false; }); CPPUNIT_ASSERT(ok); // check what we sequenced to double elapsed = globals->get_sim_time_sec(); ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { if (fp->currentIndex() == 2) { return true; } return false; }); CPPUNIT_ASSERT(ok); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); elapsed = globals->get_sim_time_sec(); ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { if (fp->currentIndex() == 3) { return true; } return false; }); CPPUNIT_ASSERT(ok); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); elapsed = globals->get_sim_time_sec(); ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { if (fp->currentIndex() == 4) { return true; } return false; }); CPPUNIT_ASSERT(ok); CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, m_gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05); ok = FGTestApi::runForTimeWithCheck(180.0, [fp] () { if (fp->currentIndex() == 5) { return true; } return false; }); CPPUNIT_ASSERT(ok); CPPUNIT_ASSERT_EQUAL(std::string{"TLA"}, fp->legAtIndex(5)->waypoint()->ident()); CPPUNIT_ASSERT_EQUAL(std::string{"TLA"}, std::string{m_gpsNode->getStringValue("wp/wp[1]/ID")}); }