Insights on Modern Control Theory

Sep 14, 2024

Lecture Notes on Modern Control Theory and State Space Modeling

Overview

  • Continuation from previous class on state space modeling in modern control theory.
  • Discussion on advantages of modern control theory.
  • Introduction of examples: LRC circuit and full state feedback or pole placement.

Modern Control Theory

  • Advantages:
    • Provides time-domain analysis.
    • Effective for highly non-linear systems.
    • Optimization capabilities (e.g., minimizing fuel).
  • Key equations:
    • State equation: ẋ = Ax + Bu
    • Output equation: Y = Cx + Du

Block Diagram Representation

  • represents the derivative of the state vector.
  • Integration of gives the state x.
  • Input u is summed with Ax to represent the system dynamics.
  • Output Y is derived from the state Cx and feedforward Du.

LRC Circuit Example

  • Description of LRC circuit components: Resistance (R), Inductance (L), Capacitance (C).
  • States defined for LRC circuit:
    • State 1: I (current)
    • State 2: Vc (voltage across capacitor)
  • Key equations derived from circuit relations:
    • V1 = VR + VL + VC
    • VR = IR, VL = L (di/dt), VC = (1/C) ∫i dt
  • State space representation:
    • ẋ = Ax + Bu where:
      • A matrix:

        [ A = \begin{bmatrix} -\frac{R}{L} & -\frac{1}{L} \ \frac{1}{C} & 0 \end{bmatrix} ]

      • Input vector: u

Full State Feedback or Pole Placement

  • Definition of full state feedback:
    • Feedback includes all states (regardless of the number).
  • Purpose of pole placement:
    • To stabilize the system by placing poles in the left half of the complex plane.
  • Control law example:
    • u = -Kx leads to modified state equation: ẋ = (A - BK)x.
  • Importance of eigenvalues and system stability:
    • Closed-loop eigenvalues determine stability.

Examples and Analyses

  • Example of transfer function: 1/(s - 1)
    • Initially unstable, poles in right half-plane.
    • By adjusting gain k, stability can be achieved.
  • Discussion on aircraft model complexity and state counts:
    • Aircraft can have higher-order state matrices (e.g., 12 states for full dynamics).
    • Control strategies can often be simplified to fewer states.

Conclusion and Next Steps

  • Modern vs. Classical Control Theory:
    • Each approach has its advantages for different situations.
  • Upcoming topics:
    • Real-time implementation in MATLAB.
    • Linearization of systems using Taylor series and Jacobian methods.
  • Importance of feedback and gains in controlling system response.
  • Next class will focus on practical examples in control system design.