UAV Flight & LQR Controller Simulation

State-Space Optimal Control (Linear-Quadratic Regulator)

X Pos: 0.00 m | Alt: 0.00 m
Pitch Angle: 0.00°
Thrust: 0.00 N | Moment: 0.00 Nm

Flight Setpoints

Lateral LQR Gains ($u_1 = -K \cdot \Delta x$)