commit
1158bb4222
@ -13,9 +13,6 @@
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// qtrocket headers
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#include "QtRocket.h"
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#include "gui/MainWindow.h"
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#include "sim/ConstantAtmosphere.h"
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#include "sim/ConstantGravityModel.h"
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// Initialize static member data
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QtRocket* QtRocket::instance = nullptr;
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@ -90,9 +90,8 @@ void MainWindow::on_testButton2_clicked()
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double initialVelocityX = initialVelocity * std::cos(initialAngle / 57.2958);
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double initialVelocityZ = initialVelocity * std::sin(initialAngle / 57.2958);
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std::shared_ptr<Rocket> rocket = std::make_shared<Rocket>();
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QtRocket::getInstance()->addRocket(rocket);
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std::vector<double> initialState = {0.0, 0.0, 0.0, initialVelocityX, 0.0, initialVelocityZ, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0};
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auto rocket = QtRocket::getInstance()->getRocket();
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rocket->setInitialState(initialState);
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rocket->setMass(mass);
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rocket->setDragCoefficient(dragCoeff);
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@ -111,14 +110,14 @@ void MainWindow::on_loadRSE_button_clicked()
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"/home",
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tr("Rocksim Engine Files (*.rse)"));
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utils::RSEDatabaseLoader loader(rseFile.toStdString());
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rseDatabase.reset(new utils::RSEDatabaseLoader(rseFile.toStdString()));
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ui->rocketPartButtons->findChild<QLineEdit*>(QString("databaseFileLine"))->setText(rseFile);
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QComboBox* engineSelector =
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ui->rocketPartButtons->findChild<QComboBox*>(QString("engineSelectorComboBox"));
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const std::vector<model::MotorModel>& motors = loader.getMotors();
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const std::vector<model::MotorModel>& motors = rseDatabase->getMotors();
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for(const auto& motor : motors)
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{
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std::cout << "Adding: " << motor.data.commonName << std::endl;
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@ -146,3 +145,13 @@ void MainWindow::on_actionSimulation_Options_triggered()
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}
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void MainWindow::on_setMotor_clicked()
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{
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QString motorName = ui->engineSelectorComboBox->currentText();
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model::MotorModel mm = rseDatabase->getMotorModelByName(motorName.toStdString());
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QtRocket::getInstance()->getRocket()->setMotorModel(mm);
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}
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@ -4,6 +4,7 @@
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/// \cond
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// C headers
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// C++ headers
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#include <memory>
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// 3rd Party headers
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#include <QMainWindow>
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/// \endcond
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@ -12,6 +13,7 @@
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#include "QtRocket.h"
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#include "gui/SimOptionsWindow.h"
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#include "utils/RSEDatabaseLoader.h"
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QT_BEGIN_NAMESPACE
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@ -47,10 +49,13 @@ private slots:
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void on_actionSimulation_Options_triggered();
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void on_setMotor_clicked();
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private:
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Ui::MainWindow* ui;
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QtRocket* qtRocket;
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SimOptionsWindow* simOptionsWindow{nullptr};
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std::unique_ptr<utils::RSEDatabaseLoader> rseDatabase;
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};
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#endif // MAINWINDOW_H
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@ -211,6 +211,13 @@
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<item row="1" column="0">
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<widget class="QComboBox" name="engineSelectorComboBox"/>
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</item>
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<item row="1" column="1">
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<widget class="QPushButton" name="setMotor">
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<property name="text">
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<string>Set Motor</string>
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</property>
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</widget>
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</item>
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</layout>
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</widget>
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<widget class="QPushButton" name="getTCMotorData">
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@ -1,14 +1,64 @@
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/// \cond
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// C headers
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// C++ headers
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#include <memory>
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// 3rd party headers
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/// \endcond
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// qtrocket headers
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#include "QtRocket.h"
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#include "SimOptionsWindow.h"
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#include "ui_SimOptionsWindow.h"
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#include "sim/SimulationOptions.h"
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SimOptionsWindow::SimOptionsWindow(QWidget *parent) :
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QMainWindow(parent),
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ui(new Ui::SimOptionsWindow)
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{
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ui->setupUi(this);
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// populate the combo boxes
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std::shared_ptr<sim::SimulationOptions> options(new sim::SimulationOptions);
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std::vector<std::string> atmosphereModels = options->getAvailableAtmosphereModels();
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std::vector<std::string> gravityModels = options->getAvailableGravityModels();
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for(const auto& i : atmosphereModels)
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{
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ui->atmosphereModelCombo->addItem(QString::fromStdString(i));
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}
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for(const auto& i : gravityModels)
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{
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ui->gravityModelCombo->addItem(QString::fromStdString(i));
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}
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}
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SimOptionsWindow::~SimOptionsWindow()
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{
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delete ui;
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}
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void SimOptionsWindow::on_buttonBox_rejected()
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{
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this->close();
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}
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void SimOptionsWindow::on_buttonBox_accepted()
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{
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QtRocket* qtrocket = QtRocket::getInstance();
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std::shared_ptr<sim::SimulationOptions> options(new sim::SimulationOptions);
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options->setTimeStep(ui->timeStep->text().toDouble());
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options->setGravityModel(ui->gravityModelCombo->currentText().toStdString());
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options->setAtmosphereModel(ui->atmosphereModelCombo->currentText().toStdString());
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qtrocket->setSimulationOptions(options);
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this->close();
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}
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explicit SimOptionsWindow(QWidget *parent = nullptr);
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~SimOptionsWindow();
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private slots:
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void on_buttonBox_rejected();
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void on_buttonBox_accepted();
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private:
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Ui::SimOptionsWindow *ui;
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};
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@ -26,7 +26,7 @@
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<x>60</x>
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<y>20</y>
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<width>261</width>
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<height>131</height>
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<height>156</height>
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</rect>
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</property>
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<layout class="QFormLayout" name="formLayout">
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@ -9,6 +9,7 @@
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#include "model/MotorModel.h"
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#include "utils/math/Constants.h"
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#include "utils/math/UtilityMathFunctions.h"
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#include "utils/Logger.h"
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namespace model
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{
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@ -69,6 +70,22 @@ double MotorModel::getMass(double simTime) const
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}
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}
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double MotorModel::getThrust(double simTime)
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{
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if(simTime > thrust.getMaxTime() + ignitionTime)
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{
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if(!burnOutOccurred)
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{
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utils::Logger::getInstance()->info("motor burnout occurred: " + std::to_string(simTime));
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burnOutOccurred = true;
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}
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return 0.0;
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}
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utils::Logger::getInstance()->info("simTime: " + std::to_string(simTime) + ": thrust: " + std::to_string(thrust.getThrust(simTime)));
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return thrust.getThrust(simTime);
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}
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void MotorModel::setMetaData(const MetaData& md)
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{
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data = md;
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@ -396,11 +396,13 @@ public:
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void startMotor(double startTime) { ignitionOccurred = true; ignitionTime = startTime; }
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void addThrustCurve(const ThrustCurve& tc) { thrust = tc; }
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// Thrust parameters
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MetaData data;
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private:
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bool ignitionOccurred{false};
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bool burnOutOccurred{false};
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double emptyMass;
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double isp;
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double maxTime;
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@ -9,6 +9,9 @@ Rocket::Rocket() : propagator(this)
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void Rocket::launch()
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{
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propagator.setTimeStep(QtRocket::getInstance()->getTimeStep());
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propagator.clearStates();
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propagator.setCurrentTime(0.0);
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mm.startMotor(0.0);
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propagator.runUntilTerminate();
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}
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@ -28,10 +31,5 @@ bool Rocket::terminateCondition(const std::pair<double, std::vector<double>>& co
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double Rocket::getThrust(double t)
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{
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return tc.getThrust(t);
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}
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void Rocket::setThrustCurve(const ThrustCurve& curve)
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{
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tc = curve;
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return mm.getThrust(t);
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}
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@ -114,7 +114,6 @@ private:
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double mass; /// @todo get rid of this, should be dynamically computed, but is the current rocket mass
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model::MotorModel mm; /// Current Motor Model
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ThrustCurve tc; /// @todo get rid of this, should be returned from the MotorModel
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};
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@ -55,12 +55,6 @@ void ThrustCurve::setIgnitionTime(double t)
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double ThrustCurve::getThrust(double t)
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{
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// calculate t relative to the start time of the motor
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static bool burnout{false};
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if(!burnout && t >= (maxTime + ignitionTime))
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{
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burnout = true;
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utils::Logger::getInstance()->info("Motor burnout at time: " + std::to_string(t));
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}
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t -= ignitionTime;
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if(t < 0.0 || t > maxTime)
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{
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@ -2,6 +2,7 @@
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/// \cond
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// C headers
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// C++ headers
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#include <cmath>
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#include <chrono>
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#include <iostream>
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#include <sstream>
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@ -97,20 +98,20 @@ double Propagator::getMass()
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double Propagator::getForceX()
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{
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QtRocket* qtrocket = QtRocket::getInstance();
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return - qtrocket->getAtmosphereModel()->getDensity(currentState[3])/ 2.0 * 0.008107 * rocket->getDragCoefficient() * currentState[3]* currentState[3];
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return (currentState[3] >= 0 ? -1.0 : 1.0) * qtrocket->getAtmosphereModel()->getDensity(currentState[2])/ 2.0 * 0.008107 * rocket->getDragCoefficient() * currentState[3]* currentState[3];
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}
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double Propagator::getForceY()
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{
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QtRocket* qtrocket = QtRocket::getInstance();
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return -qtrocket->getAtmosphereModel()->getDensity(currentState[3]) / 2.0 * 0.008107 * rocket->getDragCoefficient() * currentState[4]* currentState[4];
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return (currentState[4] >= 0 ? -1.0 : 1.0) * qtrocket->getAtmosphereModel()->getDensity(currentState[2]) / 2.0 * 0.008107 * rocket->getDragCoefficient() * currentState[4]* currentState[4];
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}
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double Propagator::getForceZ()
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{
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QtRocket* qtrocket = QtRocket::getInstance();
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double gravity = (qtrocket->getGravityModel()->getAccel(currentState[0], currentState[1], currentState[2])).x3;
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double airDrag = -qtrocket->getAtmosphereModel()->getDensity(currentState[3]) / 2.0 * 0.008107 * rocket->getDragCoefficient() * currentState[5]* currentState[5];
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double airDrag = (currentState[5] >= 0 ? -1.0 : 1.0) * qtrocket->getAtmosphereModel()->getDensity(currentState[2]) / 2.0 * 0.008107 * rocket->getDragCoefficient() * currentState[5]* currentState[5];
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double thrust = rocket->getThrust(currentTime);
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return gravity + airDrag + thrust;
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}
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@ -51,6 +51,9 @@ public:
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const std::vector<std::pair<double, std::vector<double>>>& getStates() const { return states; }
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void clearStates() { states.clear(); }
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void setCurrentTime(double t) { currentTime = t; }
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void setTimeStep(double ts) { timeStep = ts; }
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void setSaveStats(bool s) { saveStates = s; }
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@ -4,6 +4,7 @@
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/// \cond
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// C headers
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// C++ headers
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#include <algorithm>
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#include <map>
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#include <memory>
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#include <string>
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@ -42,6 +43,22 @@ public:
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SimulationOptions& operator=(const SimulationOptions&) = delete;
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SimulationOptions& operator=(SimulationOptions&&) = delete;
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std::vector<std::string> getAvailableGravityModels()
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{
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std::vector<std::string> retVal(gravityModels.size());
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std::transform(gravityModels.begin(), gravityModels.end(), std::back_inserter(retVal),
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[](auto& i) { return i.first; });
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return retVal;
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}
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std::vector<std::string> getAvailableAtmosphereModels()
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{
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std::vector<std::string> retVal(atmosphereModels.size());
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std::transform(atmosphereModels.begin(), atmosphereModels.end(), std::back_inserter(retVal),
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[](auto& i) { return i.first; });
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return retVal;
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}
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void setTimeStep(double t) { timeStep = t; }
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void setGravityModel(const std::string& model)
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{
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@ -62,16 +79,20 @@ public:
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if(model == "Constant Atmosphere")
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{
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atmosphereModel = model;
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atmosphereModels[gravityModel].reset(new sim::ConstantAtmosphere);
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atmosphereModels[atmosphereModel].reset(new sim::ConstantAtmosphere);
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}
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else if(model == "US Standard 1976")
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{
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atmosphereModel = model;
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atmosphereModels[gravityModel].reset(new sim::USStandardAtmosphere);
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atmosphereModels[atmosphereModel].reset(new sim::USStandardAtmosphere);
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}
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}
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std::shared_ptr<sim::AtmosphericModel> getAtmosphericModel() { return atmosphereModels[atmosphereModel]; }
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std::shared_ptr<sim::AtmosphericModel> getAtmosphericModel()
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{
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auto retVal = atmosphereModels[atmosphereModel];
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return retVal;
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}
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std::shared_ptr<sim::GravityModel> getGravityModel() { return gravityModels[gravityModel]; }
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double getTimeStep() { return timeStep; }
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@ -3,6 +3,7 @@
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// C headers
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// C++ headers
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#include <iostream>
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#include <algorithm>
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#include <cmath>
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// 3rd party headers
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@ -12,6 +13,7 @@
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// qtrocket headers
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#include "utils/RSEDatabaseLoader.h"
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#include "QtRocket.h"
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#include "Logger.h"
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namespace utils {
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@ -33,6 +35,19 @@ RSEDatabaseLoader::RSEDatabaseLoader(const std::string& filename)
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RSEDatabaseLoader::~RSEDatabaseLoader()
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{}
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model::MotorModel RSEDatabaseLoader::getMotorModelByName(const std::string &name)
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{
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auto mm = std::find_if(motors.begin(), motors.end(),
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[&name](const auto& i) { return name == i.data.commonName; });
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if(mm == motors.end())
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{
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Logger::getInstance()->error("Unable to locate " + name + " in RSE database");
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return model::MotorModel();
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}
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return *mm;
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}
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void RSEDatabaseLoader::buildAndAppendMotorModel(boost::property_tree::ptree& v)
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{
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model::MotorModel::MetaData mm;
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@ -70,7 +85,9 @@ void RSEDatabaseLoader::buildAndAppendMotorModel(boost::property_tree::ptree& v)
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thrustData.push_back(std::make_pair(tdata, fdata));
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}
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ThrustCurve tc(thrustData);
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model::MotorModel motorModel;
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motorModel.addThrustCurve(tc);
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motorModel.moveMetaData(std::move(mm));
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motors.emplace_back(std::move(motorModel));
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}
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|
@ -23,7 +23,9 @@ public:
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RSEDatabaseLoader(const std::string& filename);
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~RSEDatabaseLoader();
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const std::vector<model::MotorModel>& getMotors() const { return motors; }
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std::vector<model::MotorModel>& getMotors() { return motors; }
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model::MotorModel getMotorModelByName(const std::string& name);
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private:
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std::vector<model::MotorModel> motors;
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Loading…
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Reference in New Issue
Block a user