System Order & Presets
System Matrices
Matrix A (NxN)
Matrix B (Nx1)
Matrix C (1xN)
D (scalar)
Desired Closed-Loop Poles
Real parts (comma-separated)
e.g.: -2,-3 (stable poles in left-half plane)
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Controllability Rank
—
Observability Rank
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Open-Loop Stability
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Closed-Loop Stability
State Space Fundamentals
$$\dot{x} = Ax + Bu, \quad y = Cx + Du$$
Controllability: $\mathcal{C} = [B \;|\; AB \;|\; A^2B \;|\; \ldots]$ — full rank required
Observability: $\mathcal{O} = [C;\; CA;\; CA^2;\; \ldots]^T$ — full rank required
Transfer function: $H(s) = C(sI-A)^{-1}B + D$
Engineering Note: In structural FEM, mass and stiffness matrices define the state-space model. Active vibration control (active dampers, piezo actuators) uses state feedback. If certain modes are unobservable from sensor placement, they cannot be controlled regardless of actuator power.