Overview
Advanced control algorithms are the core of drone performance optimization. In this project, you will learn how to implement LQR and MPC control algorithms to improve drone flight stability and response speed.
What You’ll Learn
- LQR (Linear Quadratic Regulator) principles
- MPC (Model Predictive Control) principles
- System modeling and identification
- Controller design and implementation
Materials Needed
| Item | Quantity | Notes |
|---|---|---|
| Fully Assembled Drone | 1 | - |
| Computer | 1 | With VS Code + ESP-IDF environment |
| USB Cable | 1 | For programming |
| MATLAB or Python | 1 | For algorithm design and simulation |
Step 1: Understand Advanced Control Algorithms
LQR (Linear Quadratic Regulator)
Design optimal controllers by minimizing quadratic cost functions.
MPC (Model Predictive Control)
Predict future states based on system models and optimize control sequences.
Step 2: System Modeling
- Establish linearized model of the drone
- Include attitude dynamics and position dynamics
- Use MATLAB or Python for system identification and model validation
Step 3: Algorithm Design
Use MATLAB’s lqr() function or Python’s control library to design LQR controller:
from control import lqr
# System matrices
A = [[...]] # State matrix
B = [[...]] # Input matrix
Q = [[...]] # State weight matrix
R = [[...]] # Control weight matrix
# Calculate LQR gain
K, S, E = lqr(A, B, Q, R)
Step 4: Code Implementation
Create a new controller file in components/core/crazyflie/modules/src/controller:
// controller_lqr.c
void controllerLQR(control_t *control, setpoint_t *setpoint, const state_t *state) {
// Calculate state error
float error[12];
error[0] = setpoint->position.x - state->position.x;
error[1] = setpoint->position.y - state->position.y;
error[2] = setpoint->position.z - state->position.z;
// ... other state errors
// LQR control law: u = -K * error
float control_output[4];
for (int i = 0; i < 4; i++) {
control_output[i] = 0;
for (int j = 0; j < 12; j++) {
control_output[i] -= K[i][j] * error[j];
}
}
// Apply control output
control->thrust = control_output[0];
control->roll = control_output[1];
control->pitch = control_output[2];
control->yaw = control_output[3];
}
Step 5: Compile, Flash and Test
- Compile and flash the code
- Flight test, compare performance differences between advanced controller and PID controller
Troubleshooting
Controller unstable
- Check if system model is accurate
- Adjust weight matrices Q and R
Slow response
- Increase state weight Q
- Decrease control weight R
Achievement
Congratulations! You have implemented advanced control algorithms, which is the core technology of drone control!
Next Steps
In the next project, you will learn how to develop multi-sensor data fusion systems.