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https://gitlab.com/lander-team/lander-cpp.git
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69 lines
1.8 KiB
C++
69 lines
1.8 KiB
C++
#define M_PI 3.14159265359
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#include <cmath>
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#include <fstream>
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#include <iostream>
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#include <stdexcept> // std::runtime_error
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#include <stdio.h>
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#include <string>
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#include <vector>
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#include "Vehicle.h"
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#include "sim.h"
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bool sim(struct Vehicle &);
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int main() {
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Vehicle State;
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Vehicle PrevState;
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// PID Gains
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State.Kp = -6.8699;
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State.Ki = 0;
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State.Kd = -0.775;
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// Initial Velocity
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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 = 75 * M_PI / 180; // [rad]
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State.pitch = 30 * 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 = 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 = 7; // [degs]
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State.maxServoRate = 360; // [degs/sec]
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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 = 1; // [ms]
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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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std::cout << std::endl << "Simulation Complete 🚀" << std::endl;
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// ^^^
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// 50% chance this makes Mattys linux crash
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return 0;
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} |