2019-04-19 11:26:07 +00:00
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#include "test_routeManager.hxx"
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#include <memory>
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#include <cstring>
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#include "test_suite/FGTestApi/globals.hxx"
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#include "test_suite/FGTestApi/NavDataCache.hxx"
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#include "test_suite/FGTestApi/TestPilot.hxx"
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#include <Navaids/FlightPlan.hxx>
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#include <Navaids/NavDataCache.hxx>
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#include <Navaids/navrecord.hxx>
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#include <Navaids/navlist.hxx>
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// we need a default GPS instrument, hard to test seperately for now
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#include <Instrumentation/gps.hxx>
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#include <Autopilot/route_mgr.hxx>
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using namespace flightgear;
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static FlightPlanRef makeTestFP(const std::string& depICAO, const std::string& depRunway,
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const std::string& destICAO, const std::string& destRunway,
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const std::string& waypoints)
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{
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FlightPlanRef f = new FlightPlan;
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FGTestApi::setUp::populateFPWithNasal(f, depICAO, depRunway, destICAO, destRunway, waypoints);
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return f;
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}
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// Set up function for each test.
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void RouteManagerTests::setUp()
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{
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FGTestApi::setUp::initTestGlobals("routemanager");
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FGTestApi::setUp::initNavDataCache();
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globals->add_new_subsystem<FGRouteMgr>();
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// setup the default GPS, which is needed for waypoint
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// sequencing to work
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SGPropertyNode_ptr configNode(new SGPropertyNode);
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configNode->setStringValue("name", "gps");
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configNode->setIntValue("number", 0);
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GPS* gps(new GPS(configNode, true /* default mode */));
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m_gps = gps;
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SGPropertyNode_ptr node = globals->get_props()->getNode("instrumentation", true)->getChild("gps", 0, true);
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// node->setBoolValue("serviceable", true);
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// globals->get_props()->setDoubleValue("systems/electrical/outputs/gps", 6.0);
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globals->add_subsystem("gps", gps, SGSubsystemMgr::POST_FDM);
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globals->get_subsystem_mgr()->bind();
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globals->get_subsystem_mgr()->init();
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FGTestApi::setUp::initStandardNasal();
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globals->get_subsystem_mgr()->postinit();
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}
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// Clean up after each test.
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void RouteManagerTests::tearDown()
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{
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m_gps = nullptr;
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FGTestApi::tearDown::shutdownTestGlobals();
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}
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void RouteManagerTests::setPositionAndStabilise(const SGGeod& g)
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{
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FGTestApi::setPosition(g);
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for (int i=0; i<60; ++i) {
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globals->get_subsystem_mgr()->update(0.02);
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}
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}
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void RouteManagerTests::testBasic()
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{
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2019-09-18 22:47:13 +00:00
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//FGTestApi::setUp::logPositionToKML("rm_basic");
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2019-04-19 11:26:07 +00:00
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FlightPlanRef fp1 = makeTestFP("EGLC", "27", "EHAM", "06",
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"CLN IDESI RINIS VALKO RIVER RTM EKROS");
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fp1->setIdent("testplan");
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fp1->setCruiseFlightLevel(360);
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auto rm = globals->get_subsystem<FGRouteMgr>();
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rm->setFlightPlan(fp1);
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auto gpsNode = globals->get_props()->getNode("instrumentation/gps", true);
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CPPUNIT_ASSERT(!strcmp("obs", gpsNode->getStringValue("mode")));
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rm->activate();
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CPPUNIT_ASSERT(fp1->isActive());
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// Nasal deleagte should have placed GPS into leg mode
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auto rmNode = globals->get_props()->getNode("autopilot/route-manager", true);
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CPPUNIT_ASSERT(!strcmp("leg", gpsNode->getStringValue("mode")));
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CPPUNIT_ASSERT(!strcmp("EGLC", rmNode->getStringValue("departure/airport")));
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CPPUNIT_ASSERT(!strcmp("27", rmNode->getStringValue("departure/runway")));
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CPPUNIT_ASSERT(!strcmp("", rmNode->getStringValue("departure/sid")));
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CPPUNIT_ASSERT(!strcmp("London City", rmNode->getStringValue("departure/name")));
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CPPUNIT_ASSERT(!strcmp("EHAM", rmNode->getStringValue("destination/airport")));
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CPPUNIT_ASSERT(!strcmp("06", rmNode->getStringValue("destination/runway")));
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CPPUNIT_ASSERT_EQUAL(360, rmNode->getIntValue("cruise/flight-level"));
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CPPUNIT_ASSERT_EQUAL(false, rmNode->getBoolValue("airborne"));
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CPPUNIT_ASSERT_EQUAL(0, rmNode->getIntValue("current-wp"));
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auto wp0Node = rmNode->getNode("wp");
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CPPUNIT_ASSERT(!strcmp("EGLC-27", wp0Node->getStringValue("id")));
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auto wp1Node = rmNode->getNode("wp[1]");
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CPPUNIT_ASSERT(!strcmp("CLN", wp1Node->getStringValue("id")));
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FGPositioned::TypeFilter f{FGPositioned::VOR};
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auto clactonVOR = fgpositioned_cast<FGNavRecord>(FGPositioned::findClosestWithIdent("CLN", SGGeod::fromDeg(0.0, 51.0), &f));
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// verify hold entry course
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auto pilot = SGSharedPtr<FGTestApi::TestPilot>(new FGTestApi::TestPilot);
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FGTestApi::setPosition(fp1->departureRunway()->geod());
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pilot->resetAtPosition(fp1->departureRunway()->geod());
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pilot->setSpeedKts(220);
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pilot->setCourseTrue(fp1->departureRunway()->headingDeg());
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pilot->setTargetAltitudeFtMSL(10000);
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bool ok = FGTestApi::runForTimeWithCheck(30.0, [rmNode] () {
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if (rmNode->getIntValue("current-wp") == 1) return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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// continue outbound for some time
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pilot->setSpeedKts(250);
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FGTestApi::runForTime(30.0);
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// turn towards Clacton VOR
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pilot->flyDirectTo(clactonVOR->geod());
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pilot->setTargetAltitudeFtMSL(30000);
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pilot->setSpeedKts(280);
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ok = FGTestApi::runForTimeWithCheck(6000.0, [rmNode] () {
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if (rmNode->getIntValue("current-wp") == 2) return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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// short straight leg for testing
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pilot->flyHeading(90.0);
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pilot->setSpeedKts(330);
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FGTestApi::runForTime(30.0);
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// let's engage LNAV mode :)
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pilot->flyGPSCourse(m_gps);
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ok = FGTestApi::runForTimeWithCheck(6000.0, [rmNode] () {
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if (rmNode->getIntValue("current-wp") == 5) return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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// check where we are - should be heading to RIVER from VALKO
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CPPUNIT_ASSERT_EQUAL(5, rmNode->getIntValue("current-wp"));
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CPPUNIT_ASSERT(!strcmp("RIVER", wp0Node->getStringValue("id")));
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CPPUNIT_ASSERT(!strcmp("RTM", wp1Node->getStringValue("id")));
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// slightly rapid descent
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pilot->setTargetAltitudeFtMSL(3000);
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ok = FGTestApi::runForTimeWithCheck(6000.0, [rmNode] () {
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if (rmNode->getIntValue("current-wp") == 7) return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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// run until the GPS reverts to OBS mode at the end of the flight plan
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ok = FGTestApi::runForTimeWithCheck(6000.0, [gpsNode] () {
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std::string mode = gpsNode->getStringValue("mode");
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if (mode == "obs") return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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CPPUNIT_ASSERT_EQUAL(-1, fp1->currentIndex());
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CPPUNIT_ASSERT(!fp1->isActive());
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CPPUNIT_ASSERT_EQUAL(-1, rmNode->getIntValue("current-wp"));
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CPPUNIT_ASSERT_EQUAL(false, rmNode->getBoolValue("active"));
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}
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void RouteManagerTests::testDefaultSID()
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{
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FlightPlanRef fp1 = makeTestFP("EGLC", "27", "EHAM", "24",
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"CLN IDRID VALKO");
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fp1->setIdent("testplan");
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auto rm = globals->get_subsystem<FGRouteMgr>();
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rm->setFlightPlan(fp1);
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auto rmNode = globals->get_props()->getNode("autopilot/route-manager", true);
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rmNode->setStringValue("departure/sid", "DEFAULT");
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// let's see what we got :)
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rm->activate();
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CPPUNIT_ASSERT(fp1->isActive());
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}
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2019-09-18 22:54:32 +00:00
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void RouteManagerTests::testDirectToLegOnFlightplanAndResume()
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{
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// FGTestApi::setUp::logPositionToKML("rm_dto_resume_leg");
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// this is very similar to the identiucally name dtest in GPSTests, but relies on the Nasal
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// route manager delegate to perform the same task
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FlightPlanRef fp1 = makeTestFP("EBBR", "07L", "EGGD", "27",
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"NIK COA DVR TAWNY WOD");
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auto rm = globals->get_subsystem<FGRouteMgr>();
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rm->setFlightPlan(fp1);
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// FGTestApi::writeFlightPlanToKML(fp1);
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auto gpsNode = globals->get_props()->getNode("instrumentation/gps", true);
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auto rmNode = globals->get_props()->getNode("autopilot/route-manager", true);
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CPPUNIT_ASSERT(!strcmp("obs", gpsNode->getStringValue("mode")));
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rm->activate();
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CPPUNIT_ASSERT(fp1->isActive());
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FGTestApi::setPosition(fp1->departureRunway()->pointOnCenterline(0.0));
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FGTestApi::runForTime(10.0); // let the GPS stabilize
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CPPUNIT_ASSERT_EQUAL(std::string{"leg"}, std::string{gpsNode->getStringValue("mode")});
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CPPUNIT_ASSERT_EQUAL(std::string{"EBBR-07L"}, std::string{gpsNode->getStringValue("wp/wp[1]/ID")});
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CPPUNIT_ASSERT_EQUAL(0, rmNode->getIntValue("current-wp"));
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auto wp0Node = rmNode->getNode("wp");
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CPPUNIT_ASSERT(!strcmp("EBBR-07L", wp0Node->getStringValue("id")));
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auto wp1Node = rmNode->getNode("wp[1]");
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CPPUNIT_ASSERT(!strcmp("NIK", wp1Node->getStringValue("id")));
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// initiate a direct to
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SGGeod p2 = fp1->departureRunway()->pointOnCenterline(5.0* SG_NM_TO_METER);
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FGTestApi::setPosition(p2);
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auto doverVOR = fp1->legAtIndex(3)->waypoint()->source();
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double distanceToDover = SGGeodesy::distanceNm(p2, doverVOR->geod());
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double bearingToDover = SGGeodesy::courseDeg(p2, doverVOR->geod());
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CPPUNIT_ASSERT_EQUAL(std::string{"DVR"}, doverVOR->ident());
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gpsNode->setStringValue("scratch/ident", "DVR");
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gpsNode->setDoubleValue("scratch/longitude-deg", doverVOR->geod().getLongitudeDeg());
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gpsNode->setDoubleValue("scratch/latitude-deg", doverVOR->geod().getLatitudeDeg());
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gpsNode->setStringValue("command", "direct");
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CPPUNIT_ASSERT_EQUAL(std::string{"dto"}, std::string{gpsNode->getStringValue("mode")});
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// check that upon reaching DOVER, we sequence to TAWNY and resume leg mode
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// this is handled by the default delegate in Nasal
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SGGeod posNearDover = SGGeodesy::direct(p2, bearingToDover, (distanceToDover - 8.0) * SG_NM_TO_METER);
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FGTestApi::setPosition(posNearDover);
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auto pilot = SGSharedPtr<FGTestApi::TestPilot>(new FGTestApi::TestPilot);
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pilot->resetAtPosition(posNearDover);
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pilot->setSpeedKts(250);
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pilot->flyGPSCourse(m_gps);
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bool ok = FGTestApi::runForTimeWithCheck(180.0, [fp1] () {
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if (fp1->currentIndex() == 4) {
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return true;
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}
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return false;
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});
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CPPUNIT_ASSERT(ok);
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CPPUNIT_ASSERT_EQUAL(std::string{"leg"}, std::string{gpsNode->getStringValue("mode")});
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}
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2019-04-19 11:26:07 +00:00
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void RouteManagerTests::testDefaultApproach()
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{
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}
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2019-09-24 10:29:05 +00:00
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void RouteManagerTests::testHoldFromNasal()
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{
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// FGTestApi::setUp::logPositionToKML("rm_hold_from_nasal");
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// test that Nasal can set a hold-count (implicitly converting a leg
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// to a Hold waypt), configure the hold radial, and exit the hold
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FlightPlanRef fp1 = makeTestFP("NZCH", "02", "NZAA", "05L",
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"ALADA NS WB WN MAMOD KAPTI OH");
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fp1->setIdent("testplan");
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fp1->setCruiseFlightLevel(360);
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auto rm = globals->get_subsystem<FGRouteMgr>();
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rm->setFlightPlan(fp1);
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// FGTestApi::writeFlightPlanToKML(fp1);
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auto gpsNode = globals->get_props()->getNode("instrumentation/gps", true);
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CPPUNIT_ASSERT(!strcmp("obs", gpsNode->getStringValue("mode")));
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rm->activate();
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CPPUNIT_ASSERT(fp1->isActive());
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CPPUNIT_ASSERT(!strcmp("leg", gpsNode->getStringValue("mode")));
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SGGeod posEnrouteToWB = fp1->pointAlongRoute(3, -10.0);
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FGTestApi::setPositionAndStabilise(posEnrouteToWB);
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// sequence everything to the correct wp
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fp1->setCurrentIndex(3);
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// setup some hold data from Nasal. To make it more challenging,
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// do it once the wp is already active
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bool ok = FGTestApi::executeNasal(R"(
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var fp = flightplan(); # retrieve the global flightplan
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var leg = fp.getWP(3);
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leg.hold_count = 4;
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leg.hold_heading_radial_deg = 310;
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)");
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CPPUNIT_ASSERT(ok);
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// check the value updated in the leg
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CPPUNIT_ASSERT_EQUAL(4, fp1->legAtIndex(3)->holdCount());
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// check we converted to a hold
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auto wp = fp1->legAtIndex(3)->waypoint();
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auto holdWpt = static_cast<flightgear::Hold*>(wp);
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CPPUNIT_ASSERT_EQUAL(wp->type(), std::string{"hold"});
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CPPUNIT_ASSERT_DOUBLES_EQUAL(310.0, holdWpt->headingRadialDeg(), 0.5);
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// establish the test pilot at this position too
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auto pilot = SGSharedPtr<FGTestApi::TestPilot>(new FGTestApi::TestPilot);
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pilot->resetAtPosition(posEnrouteToWB);
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pilot->setSpeedKts(250);
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pilot->flyGPSCourse(m_gps);
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pilot->setCourseTrue(gpsNode->getDoubleValue("wp/leg-true-course-deg"));
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// run for a bit to stabilize everything
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FGTestApi::runForTime(5.0);
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// check we upgraded to a hold controller internally, and are flying to it :)
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auto statusNode = gpsNode->getNode("rnav-controller-status");
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CPPUNIT_ASSERT_EQUAL(std::string{"leg-to-hold"}, std::string{statusNode->getStringValue()});
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// check we're on the leg
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auto wbPos = fp1->legAtIndex(3)->waypoint()->position();
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auto nsPos = fp1->legAtIndex(2)->waypoint()->position();
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const double crsToWB = SGGeodesy::courseDeg(globals->get_aircraft_position(), wbPos);
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const double crsNSWB = SGGeodesy::courseDeg(nsPos,wbPos);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(crsToWB, gpsNode->getDoubleValue("wp/wp[1]/bearing-true-deg"), 0.5);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(crsNSWB, gpsNode->getDoubleValue("wp/leg-true-course-deg"), 0.5);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, gpsNode->getDoubleValue("wp/wp[1]/course-error-nm"), 0.05);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(0.0, gpsNode->getDoubleValue("wp/wp[1]/course-deviation-deg"), 0.5);
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// fly into the hold, should be teardrop entry
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ok = FGTestApi::runForTimeWithCheck(600.0, [statusNode] () {
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std::string s = statusNode->getStringValue();
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if (s == "entry-teardrop") return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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ok = FGTestApi::runForTimeWithCheck(600.0, [statusNode] () {
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std::string s = statusNode->getStringValue();
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if (s == "hold-inbound") return true;
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return false;
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});
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ok = FGTestApi::runForTimeWithCheck(600.0, [statusNode] () {
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std::string s = statusNode->getStringValue();
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if (s == "hold-outbound") return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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// half way through the outbound turn
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FGTestApi::runForTime(30.0);
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ok = FGTestApi::executeNasal(R"(
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setprop("/instrumentation/gps/command", "exit-hold");
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)");
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CPPUNIT_ASSERT(ok);
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// no change yet
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CPPUNIT_ASSERT_EQUAL(std::string{"hold-outbound"}, std::string{statusNode->getStringValue()});
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// then we fly inbound
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ok = FGTestApi::runForTimeWithCheck(600.0, [statusNode] () {
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std::string s = statusNode->getStringValue();
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if (s == "hold-inbound") return true;
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return false;
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});
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CPPUNIT_ASSERT(ok);
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// and then we exit
|
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|
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ok = FGTestApi::runForTimeWithCheck(600.0, [fp1] () {
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if (fp1->currentIndex() == 4) return true;
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return false;
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|
});
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CPPUNIT_ASSERT(ok);
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|
// get back on course
|
|
|
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FGTestApi::runForTime(60.0);
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}
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