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223 lines
7.5 KiB
223 lines
7.5 KiB
#include "testAeroMesh.hxx"
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#include "test_suite/FGTestApi/testGlobals.hxx"
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#include "test_suite/FGTestApi/PrivateAccessorFDM.hxx"
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#include "test_suite/FGTestApi/scene_graph.hxx"
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#include <vector>
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#include <map>
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#include <iostream>
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#include <simgear/constants.h>
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#include <simgear/misc/test_macros.hxx>
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#include <simgear/math/SGVec3.hxx>
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#include <simgear/math/SGGeod.hxx>
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#include <simgear/math/SGQuat.hxx>
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#include <simgear/math/SGGeoc.hxx>
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#include <simgear/props/props.hxx>
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#include <AIModel/AIAircraft.hxx>
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#include <AIModel/AIManager.hxx>
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#include <AIModel/performancedata.hxx>
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#include <AIModel/performancedb.hxx>
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#include "FDM/AIWake/AircraftMesh.hxx"
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#include "FDM/AIWake/AIWakeGroup.hxx"
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extern "C" {
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#include "src/FDM/LaRCsim/ls_matrix.h"
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}
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#include "FDM/JSBSim/math/FGLocation.h"
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#include "FDM/JSBSim/math/FGQuaternion.h"
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#include <Main/globals.hxx>
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using namespace std;
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using namespace JSBSim;
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double rho = 2.0E-3;
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// Set up function for each test.
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void AeroMeshTests::setUp()
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{
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FGTestApi::setUp::initTestGlobals("aeromesh");
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FGTestApi::setUp::initScenery();
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globals->get_props()->getNode("environment/density-slugft3", true)
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->setDoubleValue(rho);
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}
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// Clean up after each test.
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void AeroMeshTests::tearDown()
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{
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FGTestApi::tearDown::shutdownTestGlobals();
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}
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void AeroMeshTests::testLiftComputation()
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{
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double b = 10.0;
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double c = 2.0;
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AircraftMesh_ptr mesh = new AircraftMesh(b, c, "test");
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SGGeod geodPos = SGGeod::fromDeg(0.0, 0.0);
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SGVec3d pos;
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double vel = 100.;
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double weight = 50.;
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SGGeodesy::SGGeodToCart(geodPos, pos);
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mesh->setPosition(pos, SGQuatd::unit());
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SGPropertyNode* props = globals->get_props()->getNode("ai/models", true);
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props->setDoubleValue("acceleration-kts-hour", 0.0);
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props->setDoubleValue("deceleration-kts-hour", 0.0);
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props->setDoubleValue("climbrate-fpm", 0.0);
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props->setDoubleValue("decentrate-fpm", 0.0);
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props->setDoubleValue("rotate-speed-kts", 0.0);
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props->setDoubleValue("takeoff-speed-kts", 0.0);
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props->setDoubleValue("climb-speed-kts", 0.0);
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props->setDoubleValue("cruise-speed-kts", 0.0);
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props->setDoubleValue("decent-speed-kts", 0.0);
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props->setDoubleValue("approach-speed-kts", 0.0);
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props->setDoubleValue("touchdown-speed-kts", 0.0);
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props->setDoubleValue("taxi-speed-kts", 0.0);
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props->setDoubleValue("geometry/wing/span-ft", b);
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props->setDoubleValue("geometry/wing/chord-ft", c);
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props->setDoubleValue("geometry/weight-lbs", weight);
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globals->add_new_subsystem<PerformanceDB>(SGSubsystemMgr::POST_FDM);
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globals->get_subsystem<PerformanceDB>()->bind();
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globals->get_subsystem<PerformanceDB>()->init();
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FGAIManager *aiManager = new FGAIManager;
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FGAIAircraft *ai = new FGAIAircraft;
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ai->setGeodPos(geodPos);
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ai->setSpeed(vel * SG_FPS_TO_KT);
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ai->setPerformance("", "jet_transport");
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ai->getPerformance()->initFromProps(props);
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aiManager->attach(ai);
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AIWakeGroup wg;
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wg.AddAI(ai);
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SGVec3d force = mesh->GetForce(wg, SGVec3d(vel, 0., 0.), rho);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(force[1], 0.0, 1e-9);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(force[2], -weight, 1e-9);
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SGVec3d moment = mesh->GetMoment();
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CPPUNIT_ASSERT_DOUBLES_EQUAL(moment[0], 0.0, 1e-9);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(moment[1], -0.5*weight, 1e-9);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(moment[2], 0.0, 1e-9);
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auto accessor = FGTestApi::PrivateAccessor::FDM::Accessor();
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for (int i=1; i<= accessor.read_FDM_AIWake_WakeMesh_nelm(mesh); ++i)
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_WakeMesh_Gamma(accessor.read_FDM_AIWake_AIWakeGroup_aiWakeData(&wg, 1))[i][1],
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accessor.read_FDM_AIWake_WakeMesh_Gamma(mesh)[i][1], 1e-9);
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}
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void AeroMeshTests::testFourierLiftingLine()
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{
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double b = 10.0;
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double c = 2.0;
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double vel = 100.;
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double weight = 50.;
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auto accessor = FGTestApi::PrivateAccessor::FDM::Accessor();
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WakeMesh_ptr mesh = new WakeMesh(b, c, "testMesh");
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int N = accessor.read_FDM_AIWake_WakeMesh_nelm(mesh);
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double **mtx = nr_matrix(1, N, 1, N);
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double **coef = nr_matrix(1, N, 1, 1);
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mesh->computeAoA(vel, rho, weight);
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for (int m=1; m<=N; ++m) {
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double vm = M_PI*m/(N+1);
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double sm = sin(vm);
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coef[m][1] = c*M_PI/(2*b);
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for (int n=1; n<=N; ++n)
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mtx[m][n] = sin(n*vm)*(1.0+coef[m][1]*n/sm);
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}
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nr_gaussj(mtx, N, coef, 1);
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double S = b*c;
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double AR = b*b/S;
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double lift = 0.5*rho*S*vel*vel*coef[1][1]*M_PI*AR;
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double sinAlpha = weight / lift;
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lift *= sinAlpha;
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cout << "y, Lift (Fourier), Lift (VLM), Corrected lift (VLM)" << endl;
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for (int i=1; i<=N; ++i) {
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double y = accessor.read_FDM_AIWake_WakeMesh_elements(mesh)[i-1]->getBoundVortexMidPoint()[1];
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double theta = acos(2.0*y/b);
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double gamma = 0.0;
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for (int n=1; n<=N; ++n)
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gamma += coef[n][1]*sin(n*theta);
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gamma *= 2.0*b*vel*sinAlpha;
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cout << y << ", " << gamma << ", " << accessor.read_FDM_AIWake_WakeMesh_Gamma(mesh)[i][1] << ", "
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<< accessor.read_FDM_AIWake_WakeMesh_Gamma(mesh)[i][1] / gamma - 1.0 << endl;
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}
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nr_free_matrix(mtx, 1, N, 1, N);
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nr_free_matrix(coef, 1, N, 1, 1);
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}
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void AeroMeshTests::testFrameTransformations()
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{
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double b = 10.0;
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double c = 2.0;
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double yaw = 80. * SGD_DEGREES_TO_RADIANS;
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double pitch = 5. * SGD_DEGREES_TO_RADIANS;
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double roll = -10. * SGD_DEGREES_TO_RADIANS;
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SGQuatd orient = SGQuatd::fromYawPitchRoll(yaw, pitch, roll);
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SGGeod geodPos = SGGeod::fromDeg(45.0, 10.0);
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SGVec3d pos;
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SGGeodesy::SGGeodToCart(geodPos, pos);
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SGGeoc geoc = SGGeoc::fromCart(pos);
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FGLocation loc(geoc.getLongitudeRad(),
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geoc.getLatitudeRad(),
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geoc.getRadiusFt());
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CPPUNIT_ASSERT_DOUBLES_EQUAL(pos[0] * SG_METER_TO_FEET, loc(1), 1e-7);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(pos[1] * SG_METER_TO_FEET, loc(2), 1e-7);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(pos[2] * SG_METER_TO_FEET, loc(3), 1e-7);
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AircraftMesh_ptr mesh = new AircraftMesh(b, c, "test");
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mesh->setPosition(pos, orient);
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FGQuaternion qJ(roll, pitch, yaw);
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FGMatrix33 Tb2l = qJ.GetTInv();
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FGColumnVector3 refPos = loc.GetTec2l() * loc;
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for (int i=0; i < 4; ++i)
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CPPUNIT_ASSERT_DOUBLES_EQUAL(orient(i), qJ((i+1) % 4 + 1), 1e-9);
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auto accessor = FGTestApi::PrivateAccessor::FDM::Accessor();
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for (int i=0; i < accessor.read_FDM_AIWake_WakeMesh_nelm(mesh); ++i) {
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SGVec3d pt = accessor.read_FDM_AIWake_WakeMesh_elements(mesh)[i]->getBoundVortexMidPoint();
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FGColumnVector3 ptJ(pt[0], pt[1], pt[2]);
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FGColumnVector3 p = loc.GetTl2ec() * (refPos + Tb2l * ptJ);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_AircraftMesh_midPt(mesh)[i][0], p(1), 1e-7);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_AircraftMesh_midPt(mesh)[i][1], p(2), 1e-7);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_AircraftMesh_midPt(mesh)[i][2], p(3), 1e-7);
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pt = accessor.read_FDM_AIWake_WakeMesh_elements(mesh)[i]->getCollocationPoint();
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ptJ.InitMatrix(pt[0], pt[1], pt[2]);
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p = loc.GetTl2ec() * (refPos + Tb2l * ptJ);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_AircraftMesh_collPt(mesh)[i][0], p(1), 1e-7);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_AircraftMesh_collPt(mesh)[i][1], p(2), 1e-7);
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CPPUNIT_ASSERT_DOUBLES_EQUAL(accessor.read_FDM_AIWake_AircraftMesh_collPt(mesh)[i][2], p(3), 1e-7);
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}
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}
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