Optimal Control Design

Linear Quadratic Regulator with Kalman Filtering for Spacecraft Attitude Control

Q (State Weight)10

R (Control Weight)1

Initial Angle (deg)10

Inertia (kg·m²)100

Performance Metrics

Settling Time--

Overshoot--

Peak Torque--

∫|u|dt--

Desired Damping (ζ)0.7

Natural Freq (rad/s)1.0

Closed-Loop Poles

Pole 1--

Pole 2--

StabilityStable

Sweep Parameter

Optimal Settings

K₁ (position)--

K₂ (rate)--

Process Noise (Q_k)0.1

Measurement Noise (R_k)0.5

Estimation Error

RMS Error--

Peak Error--