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https://gitlab.com/lander-team/lander-cpp.git
synced 2025-07-23 14:41:25 +00:00
Cleaned up PID
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@@ -34,7 +34,7 @@ struct Vehicle {
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double Kp, Ki, Kd;
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double yError, yPrevError;
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double pError, pPrevError;
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double y_pidRefeed, p_pidRefeed, i_yError, i_pError = 0;
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double i_yError, i_pError = 0;
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double simTime;
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int stepSize;
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@@ -3,8 +3,8 @@
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void burnStartTimeCalc(struct Vehicle &);
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void thrustSelection(struct Vehicle &, int t);
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void lqrCalc(struct Vehicle &);
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void pidController(struct Vehicle &);
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// void lqrCalc(struct Vehicle &);
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void pidController(struct Vehicle &, struct Vehicle &);
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void TVC(struct Vehicle &);
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void vehicleDynamics(struct Vehicle &, struct Vehicle &, int t);
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void state2vec(struct Vehicle &, struct outVector &, int t);
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@@ -30,7 +30,7 @@ bool sim(struct Vehicle &State, struct Vehicle &PrevState) {
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do {
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thrustSelection(State, t);
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// lqrCalc(State);
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pidController(State);
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pidController(State, PrevState);
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TVC(State);
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vehicleDynamics(State, PrevState, t);
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state2vec(State, stateVector, t);
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@@ -179,36 +179,32 @@ void lqrCalc(Vehicle &State) {
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State.LQRy = -1 * State.thrust;
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}
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void pidController(Vehicle &State) {
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void pidController(Vehicle &State, struct Vehicle &PrevState) {
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// Not used in this function, but it was in the LQR function so had to copy it
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// over since we don't run LQR when running PID
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State.I11 = State.mass * ((1 / 12) * pow(State.vehicleHeight, 2) +
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pow(State.vehicleRadius, 2) / 4);
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State.I22 = State.mass * ((1 / 12) * pow(State.vehicleHeight, 2) +
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pow(State.vehicleRadius, 2) / 4);
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State.I33 = State.mass * 0.5 * pow(State.vehicleRadius, 2);
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if (State.thrust > 1) {
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State.yError = State.yaw; // - State.y_pidRefeed;
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State.pError = State.pitch; // - State.p_pidRefeed;
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// Make sure we start reacting when we start burning
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if (State.thrust > 0.01) {
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// Integral of Error
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State.i_yError = integral(State.yaw, State.i_yError, State.stepSize);
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State.i_pError = integral(State.pitch, State.i_pError, State.stepSize);
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State.i_yError += State.yError * State.stepSize / 1000;
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State.i_pError += State.pError * State.stepSize / 1000;
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// Derivative of Error
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double d_yError = derivative(State.yaw, PrevState.yaw, State.stepSize);
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double d_pError = derivative(State.pitch, PrevState.pitch, State.stepSize);
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double d_yError =
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(State.yError - State.yPrevError) / (State.stepSize / 1000);
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double d_pError =
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(State.pError - State.pPrevError) / (State.stepSize / 1000);
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// PID Function
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State.LQRx = (State.Kp * State.yError + State.Ki * State.i_yError +
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// PID Function - it says LQR but this is just so that it gets passed to the
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// TVC block properly
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State.LQRx = (State.Kp * State.yaw + State.Ki * State.i_yError +
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State.Kd * d_yError);
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State.LQRy = (State.Kp * State.pError + State.Ki * State.i_pError +
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State.LQRy = (State.Kp * State.pitch + State.Ki * State.i_pError +
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State.Kd * d_pError);
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// std::cout << State.LQRx << ", ";
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State.yPrevError = State.yError;
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State.pPrevError = State.pError;
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} else {
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State.LQRx = 0;
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State.LQRy = 0;
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@@ -228,7 +224,7 @@ void pidController(Vehicle &State) {
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}
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void TVC(Vehicle &State) {
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if (State.thrust < 1) {
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if (State.thrust < 0.1) {
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// Define forces and moments for t = 0
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State.Fx = 0;
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State.Fy = 0;
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@@ -313,18 +309,12 @@ void vehicleDynamics(Vehicle &State, Vehicle &PrevState, int t) {
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State.rolldot = integral(State.rollddot, PrevState.rolldot, State.stepSize);
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// ax ay az
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State.ax =
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(State.Fx /
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State.mass); // +
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//(State.pitchdot * State.vz - State.rolldot * State.vy);
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State.ay =
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(State.Fy /
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State.mass); // +
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//(State.rolldot * State.vx - State.vz * State.yawdot);
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State.az =
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(State.Fz /
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State.mass); // +
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//(State.vy * State.yawdot - State.pitchdot * State.vx);
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State.ax = (State.Fx / State.mass) +
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(State.pitchdot * State.vz - State.rolldot * State.vy);
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State.ay = (State.Fy / State.mass) +
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(State.rolldot * State.vx - State.vz * State.yawdot);
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State.az = (State.Fz / State.mass) +
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(State.vy * State.yawdot - State.pitchdot * State.vx);
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// vx vy vz in Body frame
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State.vx = integral(State.ax, PrevState.vx, State.stepSize);
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@@ -439,6 +429,7 @@ void write2CSV(outVector &stateVector, Vehicle &State) {
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}
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outfile.close();
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std::cout << "Output File Closed\n";
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}
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double derivative(double current, double previous, double step) {
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