15 Matching Annotations
  1. May 2026
    1. must be less than 1 (or 0 dB) when its phase angle is −180∘-180^{\circ} .

      Check Gain at Phase Angle = -180. The Gain needs to be smaller than 1 for stability.

      Ex: Gain is around -15 dB at -180 degrees. This is less than 1, therefore the system is stable! Corresponding Frequency: 30.9

    2. critical phase angle

      Check Phase Angle at Gain = 0 dB. This needs to be above -180 degrees.

      Ex: Phase is around -142 at 0 dB. This is more than -180, therefore the system is stable. Corresponding Frequency: 12.2 rad/s

    1. Instability occurs when1 + G(ıω) = 0

      Check the denominator of the transfer function of a unity feedback system. The system is, of course, unstable if the function is undefined.

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  2. Apr 2026
    1. time delay

      Time Delay Example:

      After energizing relay, it takes time before power reaching other end.

      Essentially, delay from signal sent to signal received to output motion carried out.

    2. .

      Transfer Function is in polynomial form, traditionally to see poles in the CE, denominator.

      When it isn't given in polynomial form, it becomes hard to find poles.

  3. Feb 2026
    1. frequency ω

      Make Bode Diagram and look at -3 dB

      Read Breakpoint Frequency, w_b $$s = a \pm jb$$

      In transfer function G(s), substitute $$s=jw_b=\frac{j}{\tau}$$

      Solve the Transfer Function

      Convert to Polar Form $$z = a + jb , $$ $$z = r \angle \theta , \quad r = \sqrt{a^2 + b^2}$$ $$ \quad \theta = \tan^{-1}!\left(\frac{b}{a}\right)$$

      $$r = k_dc$$

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    1. unity-feedback system

      No transfer function for returning pass (unity)

      Input=Output for returning pass.

      ex: cruise control. r=desired speed, y=actual speed

      • $$r-y = e$$

      • \(e\) represents the tracking error, the difference between the desired output \(r\) and the actual output \(y\).

    2. output of a PID controller

      $$ u(t) = K_p e(t) + K_i \int e(t)\,dt + K_d \frac{de}{dt} $$

      • The control signal \(u\) to the plant is equal to the proportional gain \(K_p\) times the magnitude of the error plus the integral gain \(K_i\) times the integral of the error plus the derivative gain \(K_d\) times the derivative of the error.
    1. Floating Control Mode

      When you route error into the control system.

      Example gravel depositing on weighted belt * Weight too heavy, system controls flow rate to reduce weight * Weight is sufficient, system does no work to correct error = neutral zone

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