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Formal build for Avionics Integration Test
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@ -80,7 +80,7 @@ void init_Vehicle(Vehicle &State) {
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State.momentArm = 0.145; // [m]
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// Sim Step Size
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State.stepSize = 1.0; // [ms]
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State.stepSize = 20.0; // [ms]
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// Other Properties
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State.massPropellant = 0.06; // [kg]
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@ -240,10 +240,10 @@ void printSimResults(Vehicle &State) {
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Serial.print("Final Angles: [" + String(State.yaw) + ", " +
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String(State.pitch) + "]\n");
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if (landing_velocity < 0.5) {
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Serial.print("Landing Velocity < 0.5 m/s | PASS | ");
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if (landing_velocity < 1.0) {
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Serial.print("Landing Velocity < 1.0 m/s | PASS | ");
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} else {
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Serial.print("Landing Velocity < 0.5 m/s | FAIL | ");
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Serial.print("Landing Velocity < 1.0 m/s | FAIL | ");
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}
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Serial.print("Final Velocity: [" + String(State.vx) + ", " +
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String(State.vy) + ", " + String(State.vz) + "]\n");
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@ -75,7 +75,7 @@ void setup() {
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testGimbal(servo1, servo2);
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Serial.println("Servos Tested");
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delay(1000);
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delay(3000);
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Serial.println("Simulated Vehicle Initalized");
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// Determine when to burn
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@ -104,17 +104,18 @@ void loop() {
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State.time += State.stepSize;
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if ((State.z < 0.0) && (State.thrustFiring == 2)) {
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printSimResults(State);
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Serial.println("Run duration:" + String(micros() - initTime) + " us");
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closeFile();
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delay(20000);
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delay(3000);
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Serial.println("SUCCESS");
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Serial.println("Aborting Sim");
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teensyAbort();
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}
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delay(20 - ((micros() - last) * 1000.0));
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delay(20.0 - ((micros() - last) / 1000.0));
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}
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void init_loadCells() {
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