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Merge branch 'revert-ee670776' into 'main'
Revert input file commit Closes #7 See merge request lander-team/lander-cpp!6
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commit
0d66bd0f5a
@ -48,7 +48,7 @@ title('Altitude vs Time')
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xlabel('Time (s)')
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ylabel('Altitude (m)')
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ylim([0 z(1)+5])
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%saveas(gcf,'outputs/Accel-Vel-Alt vs Time.png')
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saveas(gcf,'outputs/Accel-Vel-Alt vs Time.png')
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figure(2)
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@ -72,7 +72,7 @@ plot(t, rolldot)
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title('Angular Velocity vs Time')
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xlabel('Time (ms)')
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ylabel('Angular Velocity (deg/s)')
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%saveas(gcf,'outputs/Euler Angles vs Time.png')
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saveas(gcf,'outputs/Euler Angles vs Time.png')
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legend("yawdot", "pitchdot", "rolldot")
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figure(3)
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@ -90,4 +90,4 @@ plot(t, Servo2)
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title('Servo 2 Position vs Time')
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xlabel('Time (ms)')
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ylabel('Servo 2 Position (rad)')
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%saveas(gcf,'outputs/Servo Position vs Time.png')
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saveas(gcf,'outputs/Servo Position vs Time.png')
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88
src/main.cpp
88
src/main.cpp
@ -3,10 +3,7 @@
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#include <cmath>
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#include <fstream>
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#include <iostream>
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#include <string>
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#include <stdexcept> // std::runtime_error
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#include <stdio.h>
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#include <vector>
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#include "Vehicle.h"
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#include "sim.h"
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@ -17,67 +14,50 @@ int main() {
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Vehicle State;
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Vehicle PrevState;
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// Create an input filestream
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std::ifstream inFile("input.csv");
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// Make sure the file is open
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if (!inFile.is_open())
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throw std::runtime_error("Could not open file");
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std::vector<double> varValueVec = std::vector<double>(17, 0.0);
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std::string varName, varValue, varUnits;
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for (int i; i < 17; i++) {
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std::getline(inFile, varName, ',');
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std::getline(inFile, varValue, ',');
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varValueVec[i] = stod(varValue);
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std::getline(inFile, varUnits);
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}
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// Initial Velocity
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State.vx = varValueVec[0]; // [m/s]
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State.vy = varValueVec[1]; // [m/s]
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State.vz = varValueVec[2]; // [m/s]
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State.vx = 0; // [m/s]
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State.vy = 0; // [m/s]
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State.vz = 0; // [m/s]
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// Initial YPR
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State.yaw = varValueVec[3] * M_PI / 180; // [rad]
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State.pitch = varValueVec[4] * M_PI / 180; // [rad]
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State.roll = varValueVec[5] * M_PI / 180; // [rad]
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// Initial YPR
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State.yaw = 10 * M_PI / 180; // [rad]
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State.pitch = 5 * M_PI / 180; // [rad]
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State.roll = 0 * M_PI / 180; // [rad]
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// Initial YPRdot
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State.yawdot = varValueVec[6] * M_PI / 180; // [rad/s]
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State.pitchdot = varValueVec[7] * M_PI / 180; // [rad/s]
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State.rolldot = varValueVec[8] * M_PI / 180; // [rad/s]
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// Initial YPRdot
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State.yawdot = 1 * M_PI / 180; // [rad/s]
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State.pitchdot = -1 * M_PI / 180; // [rad/s]
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State.rolldot = 0 * M_PI / 180; // [rad/s]
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// Servo Limitation
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State.maxServo = varValueVec[9]; // [degs]
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// Servo Limitation
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State.maxServo = 15; // [degs]
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// Vehicle Properties
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State.massInitial = varValueVec[10]; // [kg]
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State.vehicleHeight = varValueVec[13]; // [m]
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State.vehicleRadius = varValueVec[14]; // [m]
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State.momentArm = varValueVec[15]; // [m]
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// Vehicle Properties
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State.massInitial = 1.2; // [kg]
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State.vehicleHeight = 0.5318; // [m]
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State.vehicleRadius = 0.05105; // [m]
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State.momentArm = 0.145; // [m]
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// Sim Step Size
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State.stepSize = varValueVec[16]; // [ms]
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// Sim Step Size
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State.stepSize = 1; // [ms]
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// Other Properties
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State.burntime = varValueVec[12]; // [s]
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State.massPropellant = varValueVec[11]; // [kg]
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State.massBurnout = State.massInitial - State.massPropellant; // [kg]
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State.mdot = State.massPropellant / State.burntime; // [kg/s]
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State.mass = State.massInitial; // [kg]
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State.burnElapsed = 2000; // [s]
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PrevState.thrust = 0; // [N]
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// Other Properties
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State.massPropellant = 0.06; // [kg]
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State.massBurnout = State.massInitial - State.massPropellant; // [kg]
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State.burntime = 3.45 - 0.148; // [s]
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State.mdot = State.massPropellant / State.burntime; // [kg/s]
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State.mass = State.massInitial; // [kg]
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State.burnElapsed = 2000; // [s]
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PrevState.thrust = 0; // [N]
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bool outcome = sim(State, PrevState);
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bool outcome = sim(State, PrevState);
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std::cout << "Finished"
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<< "\n";
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std::cout << "Finished"
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<< "\n";
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if (outcome == 1) {
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std::cout << "Sim Result = Success!";
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return 0;
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if (outcome == 1) {
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std::cout << "Sim Result = Success!";
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return 0;
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} else if (outcome == 0) {
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std::cout << "Sim Result = Failed!";
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// return 1; Until I figure out how to make CI/CD continue even when run
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