mirror of
https://gitlab.com/lander-team/lander-cpp.git
synced 2025-06-16 07:06:51 +00:00
236 lines
6.3 KiB
C
236 lines
6.3 KiB
C
#include "Vehicle.h"
|
|
#include <Arduino.h>
|
|
#include <SD.h>
|
|
#include <SPI.h>
|
|
|
|
double loadCellCalibrate();
|
|
void initFile();
|
|
void thrustInfo(struct Vehicle &);
|
|
void processTVC(struct Vehicle &);
|
|
void write2CSV(struct Vehicle &);
|
|
void printSimResults(struct Vehicle &);
|
|
void teensyAbort();
|
|
|
|
const int chipSelect = BUILTIN_SDCARD;
|
|
File dataFile;
|
|
|
|
double loadCellCalibrate() {
|
|
// place code to calibrate load cells in here
|
|
double loadTotal;
|
|
for (double t = 0; t == 10; ++t) {
|
|
loadTotal += 1;
|
|
delay(15);
|
|
}
|
|
return loadTotal / 10;
|
|
}
|
|
|
|
void initFile() {
|
|
Serial.print("Initializing SD card...");
|
|
|
|
// see if the card is present and can be initialized:
|
|
if (!SD.begin(chipSelect)) {
|
|
Serial.println("Card failed, or not present. \n\nABORTING SIMULATION");
|
|
teensyAbort();
|
|
}
|
|
Serial.println("Card initialized.");
|
|
|
|
int i = 1;
|
|
Serial.print("simOut_" + String(i) + ".csv");
|
|
const char *fileName;
|
|
|
|
if (SD.exists("simOut.csv")) {
|
|
while (i > 0) {
|
|
fileName = ("simOut_" + String(i) + ".csv").c_str();
|
|
|
|
if (!SD.exists(fileName)) {
|
|
// Open simOut_i.csv
|
|
dataFile = SD.open(fileName, FILE_WRITE);
|
|
|
|
if (dataFile) {
|
|
Serial.println("File successfully opened!");
|
|
|
|
} else {
|
|
// if the file didn't open, print an error:
|
|
Serial.println("Error opening output file. \n\nABORTING SIMULATION");
|
|
teensyAbort();
|
|
}
|
|
i = 0;
|
|
|
|
} else {
|
|
i++;
|
|
}
|
|
}
|
|
} else {
|
|
// Open simOut.csv
|
|
dataFile = SD.open("simOut.csv", FILE_WRITE);
|
|
if (dataFile) {
|
|
Serial.println("File successfully opened!");
|
|
|
|
} else {
|
|
// if the file didn't open, print an error:
|
|
Serial.println("Error opening output file. \n\nABORTING SIMULATION");
|
|
teensyAbort();
|
|
}
|
|
}
|
|
|
|
// File Header
|
|
dataFile.println(
|
|
"t,x,y,z,vx,vy,vz,ax,ay,az,yaw,pitch,roll,yawdot,pitchdot,rolldot,"
|
|
"Servo1,Servo2,thrustFiring,PIDx,PIDy,thrust");
|
|
}
|
|
|
|
void thrustInfo(Vehicle &State) {
|
|
if (State.time == 0) {
|
|
Serial.println("WARNING: thrustInfo not implemented for TEENSY");
|
|
}
|
|
|
|
if (State.burnElapsed != 2000) {
|
|
// determine where in the thrust curve we're at based on elapsed burn time
|
|
// as well as current mass
|
|
State.burnElapsed = (State.time - State.burnStart) / 1000;
|
|
State.mass = State.massInitial - (State.mdot * State.burnElapsed);
|
|
}
|
|
|
|
else if (abs(State.burnVelocity + State.vz) < 0.001) {
|
|
// Start burn
|
|
State.burnStart = State.time;
|
|
State.burnElapsed = 0;
|
|
}
|
|
|
|
else
|
|
State.burnElapsed = 2000; // arbitrary number to ensure we don't burn
|
|
|
|
if ((State.burnElapsed > 0.147) && (State.burnElapsed < 0.420)) {
|
|
State.thrustFiring = true;
|
|
State.thrust = 65.165 * State.burnElapsed - 2.3921;
|
|
|
|
} else if ((State.burnElapsed > 0.419) && (State.burnElapsed < 3.383))
|
|
State.thrust = 0.8932 * pow(State.burnElapsed, 6) -
|
|
11.609 * pow(State.burnElapsed, 5) +
|
|
60.739 * pow(State.burnElapsed, 4) -
|
|
162.99 * pow(State.burnElapsed, 3) +
|
|
235.6 * pow(State.burnElapsed, 2) -
|
|
174.43 * State.burnElapsed + 67.17;
|
|
|
|
else if ((State.burnElapsed > 3.382) && (State.burnElapsed < 3.46))
|
|
State.thrust = -195.78 * State.burnElapsed - 675.11;
|
|
|
|
if (State.burnElapsed > 3.45) {
|
|
State.thrustFiring = false;
|
|
State.thrust = 0;
|
|
}
|
|
}
|
|
|
|
void processTVC(Vehicle &State) {
|
|
if (State.time == 0) {
|
|
Serial.println("WARNING: processTVC not implemented for TEENSY");
|
|
}
|
|
|
|
// Vector math to aqcuire thrust vector components
|
|
State.Fx = State.thrust * sin(State.xServoDegs * (M_PI / 180));
|
|
State.Fy = State.thrust * sin(State.yServoDegs * (M_PI / 180));
|
|
State.Fz = sqrt(pow(State.thrust, 2) - pow(State.Fx, 2) - pow(State.Fy, 2)) +
|
|
(State.mass * g);
|
|
|
|
// Calculate moment created by Fx and Fy
|
|
State.momentX = State.Fx * State.momentArm;
|
|
State.momentY = State.Fy * State.momentArm;
|
|
State.momentZ = 0;
|
|
}
|
|
|
|
void write2CSV(Vehicle &State) {
|
|
dataFile.print(State.time);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.x);
|
|
dataFile.print(",");
|
|
dataFile.print(State.y);
|
|
dataFile.print(",");
|
|
dataFile.print(State.z);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.vx);
|
|
dataFile.print(",");
|
|
dataFile.print(State.vy);
|
|
dataFile.print(",");
|
|
dataFile.print(State.vz);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.ax);
|
|
dataFile.print(",");
|
|
dataFile.print(State.ay);
|
|
dataFile.print(",");
|
|
dataFile.print(State.az);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.yaw * 180 / M_PI);
|
|
dataFile.print(",");
|
|
dataFile.print(State.pitch * 180 / M_PI);
|
|
dataFile.print(",");
|
|
dataFile.print(State.roll * 180 / M_PI);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.yawdot * 180 / M_PI);
|
|
dataFile.print(",");
|
|
dataFile.print(State.pitchdot * 180 / M_PI);
|
|
dataFile.print(",");
|
|
dataFile.print(State.rolldot * 180 / M_PI);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.xServoDegs);
|
|
dataFile.print(",");
|
|
dataFile.print(State.yServoDegs);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.thrustFiring);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.PIDx);
|
|
dataFile.print(",");
|
|
dataFile.print(State.PIDy);
|
|
dataFile.print(",");
|
|
|
|
dataFile.print(State.thrust);
|
|
dataFile.print("\n");
|
|
}
|
|
|
|
void printSimResults(Vehicle &State) {
|
|
State.yaw = State.yaw * 180 / M_PI;
|
|
State.pitch = State.pitch * 180 / M_PI;
|
|
State.roll = State.roll * 180 / M_PI;
|
|
|
|
double landing_angle =
|
|
pow(State.yaw * State.yaw + State.pitch * State.pitch, .5);
|
|
|
|
double landing_velocity =
|
|
pow(State.vx * State.vx + State.vy * State.vy + State.vz * State.vz, .5);
|
|
|
|
if (landing_angle < 5.0) {
|
|
Serial.print("Landing Angle < 5.0 degrees | PASS | ");
|
|
} else {
|
|
Serial.print("Landing Angle < 5.0 degrees | FAIL | ");
|
|
}
|
|
Serial.print("Final Angles: [" + String(State.yaw) + ", " +
|
|
String(State.pitch) + "]\n");
|
|
|
|
if (landing_velocity < 0.5) {
|
|
Serial.print("Landing Velocity < 0.5 m/s | PASS | ");
|
|
} else {
|
|
Serial.print("Landing Velocity < 0.5 m/s | FAIL | ");
|
|
}
|
|
Serial.print("Final Velocity: [" + String(State.vx) + ", " +
|
|
String(State.vy) + ", " + String(State.vz) + "]\n");
|
|
|
|
Serial.print("\nSimulation Complete\n");
|
|
}
|
|
|
|
void closeFile() {
|
|
// close the file:
|
|
dataFile.close();
|
|
Serial.println("File closed\n");
|
|
}
|
|
|
|
void teensyAbort() {
|
|
while (1) {
|
|
}
|
|
} |