Math Problem Statement

The diagram shown in the attached image is inherently unstable. Your goal is to make the system stable by using the feedforward and phase commepensator

The diagram shown in the attached image is inherently unstable. Your goal is to make the system stable by using the feedforward and phase compensator.

Solution

To stabilize the inherently unstable system in the given block diagram, we can analyze and design a feedforward compensator and/or a phase compensator. Below is the step-by-step process for achieving stability:


1. Analyze the Open-Loop Transfer Function

The open-loop transfer function is the product of the components in the forward path: G(s)=kc1s(s1)G(s) = k_c \cdot \frac{1}{s(s-1)}

  • The pole at s=1s=1 is in the right-half plane (RHP), making the system unstable.

2. Introduce Feedforward Compensation

We need to modify the open-loop transfer function using a feedforward compensator C(s)C(s). A suitable approach is to use pole-zero cancellation or adjust the dynamics of the system.

Feedforward compensator design:

Let C(s)=s+as+bC(s) = \frac{s+a}{s+b}, where aa and bb are constants.

To counteract the instability introduced by the pole at s=1s=1, set b>1b > 1. For simplicity: C(s)=s+as+b,b>1C(s) = \frac{s+a}{s+b}, \quad b > 1

This introduces a new stable pole at s=bs = -b. The zero at s=as = -a can be adjusted to improve transient response.


3. Add Phase Compensation

To ensure stability and improve the phase margin, you can implement a phase lead compensator of the form: Clead(s)=kleads+zs+p,z>pC_{\text{lead}}(s) = k_{\text{lead}} \cdot \frac{s+z}{s+p}, \quad |z| > |p| This compensator increases the phase of the system at critical frequencies and helps stabilize the feedback system.

Typical tuning steps:

  1. Choose zero zz: Place it near the unstable pole (e.g., z=1z = 1).
  2. Choose pole pp: Place it farther left in the complex plane (e.g., p=5p = 5).

Example: Clead(s)=kleads+1s+5C_{\text{lead}}(s) = k_{\text{lead}} \cdot \frac{s+1}{s+5}

The compensator stabilizes the phase response of the system.


4. Closed-Loop Stability Verification

After adding the feedforward and phase compensator, verify the closed-loop transfer function stability. The new open-loop transfer function becomes: G(s)=C(s)G(s)=(s+as+b)kc1s(s1)G'(s) = C(s) \cdot G(s) = \left(\frac{s+a}{s+b}\right) \cdot k_c \cdot \frac{1}{s(s-1)} Analyze the poles of the closed-loop transfer function to ensure all poles are in the left-half plane (LHP).


5. Practical Guidelines

  1. Use software tools like MATLAB to simulate and verify the step response and stability.
  2. Adjust kck_c, aa, bb, zz, and pp to fine-tune the response.
  3. Ensure sufficient phase margin (typically 4545^\circ or higher) for robustness.

Would you like a MATLAB simulation or further details on compensator design?


Related Questions to Explore:

  1. What is the root-locus plot of the original system?
  2. How does the feedforward compensator affect the system’s stability?
  3. What phase margin is required to stabilize this system?
  4. How can the lead compensator improve the transient response?
  5. What is the effect of varying the controller gain kck_c on stability?

Tip:

Always verify the closed-loop poles using the characteristic equation 1+G(s)H(s)=01 + G'(s)H(s) = 0.

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Math Problem Analysis

Mathematical Concepts

Control Systems
Transfer Functions
Feedback Systems
Stability Analysis
Compensator Design

Formulas

Open-loop transfer function: G(s) = kc / (s(s - 1))
Feedforward compensator: C(s) = (s + a) / (s + b), b > 1
Phase lead compensator: Clead(s) = klead * (s + z) / (s + p), |z| > |p|
Characteristic equation: 1 + G'(s)H(s) = 0

Theorems

Root Locus Technique
Nyquist Stability Criterion
Bode Plot Analysis

Suitable Grade Level

Undergraduate Engineering (Control Systems)