Question:

The swing equation of a synchronous generator is

Show Hint

Because the swing equation is a non-linear second-order differential equation, it cannot be solved analytically. Instead, numerical techniques such as the Equal-Area Criterion or step-by-step methods (e.g., modified Euler or Runge-Kutta methods) must be used.
Updated On: Jun 25, 2026
  • Linear, second order differential equation
  • Non-linear, second order differential equation
  • Non-linear, second order algebraic equation
  • Non-linear, first order differential equation
Show Solution
collegedunia
Verified By Collegedunia

The Correct Option is B

Solution and Explanation

Concept: The swing equation governs the electromechanical rotor dynamics of a synchronous machine during transient disturbances. It balances the input mechanical power, output electromagnetic power, and accelerating power. Mathematically, the swing equation is expressed as: \[ \frac{H}{\pi f} \frac{d^2\delta}{dt^2} = P_m - P_e \] where $H$ is the inertia constant, $f$ is the system frequency, $\delta$ is the rotor power angle, $P_m$ is the mechanical shaft power input, and $P_e$ is the electrical power output.

Step 1: Analyze the order of the differential equation.

The swing equation contains the term $\frac{d^2\delta}{dt^2}$, which represents the second derivative of the rotor angle $\delta$ with respect to time $t$. This means it is mathematically classified as a second-order differential equation.

Step 2: Determine if the equation is linear or non-linear.

The electrical power output $P_e$ of a cylindrical rotor synchronous generator is given by the power-angle relation: \[ P_e = P_{max} \sin\delta \] Substituting this expression back into the structural swing equation yields: \[ \frac{H}{\pi f} \frac{d^2\delta}{dt^2} = P_m - P_{max} \sin\delta \] The presence of the transcendental function $\sin\delta$ introduces a fundamental non-linearity to the system. The variable $\delta$ cannot be separated linearly, making the differential equation non-linear. Thus, the swing equation is a non-linear, second-order differential equation. This corresponds to Option (B).
Was this answer helpful?
0
0