Give step-by-step solution with explanation and final answer:Problem 5: ElectroMechanical System
Figure P3.32 shows a schematic diagram of a solenoid actuator. Energizing the coil (armature circuit)
creates the electromagnetic force F,, that acts on the armature—valve mass m. Through experimentation
Vaughan and Gamble [6] developed the following nonlinear equation for solenoid current:
1,(3) = a; 4° + a, A (amps, A)
where A is the magnetic flux linkage (Wb) and a; and a, are constants. This nonlinear current model
accounts for back emf and the variable inductance because of the displacement of the armature mass.
Vaughan and Gamble also developed the empirical equation for electromagnetic force:
Fon) = 2° + ¢,4* + 0,2 (N)
where cg, ¢,, and ¢, are empirical constants from experiments. Derive the complete mathematical model
of the electromechanical actuator. Assume that the return spring is undeflected when x = 0 and the elec-
tromagnetic force is zero.
R
x N
= Return sj
+ G pring,
4 Fe; k
N N
‘Armature circuit \—— —— Viscous friction, &
Armature + valve mass
Figure P3.32
Question:
Give step-by-step solution with explanation and final answer:Problem 5: ElectroMechanical System
Figure P3.32 shows a schematic diagram of a solenoid actuator. Energizing the coil (armature circuit)
creates the electromagnetic force F,, that acts on the armature—valve mass m. Through experimentation
Vaughan and Gamble [6] developed the following nonlinear equation for solenoid current:
1,(3) = a; 4° + a, A (amps, A)
where A is the magnetic flux linkage (Wb) and a; and a, are constants. This nonlinear current model
accounts for back emf and the variable inductance because of the displacement of the armature mass.
Vaughan and Gamble also developed the empirical equation for electromagnetic force:
Fon) = 2° + ¢,4* + 0,2 (N)
where cg, ¢,, and ¢, are empirical constants from experiments. Derive the complete mathematical model
of the electromechanical actuator. Assume that the return spring is undeflected when x = 0 and the elec-
tromagnetic force is zero.
R
x N
= Return sj
+ G pring,
4 Fe; k
N N
‘Armature circuit \—— —— Viscous friction, &
Armature + valve mass
Figure P3.32
This is AI generated Response.
Asked by: hhhh
Created at: 2025-05-28 10:04:05
Final Answer:
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Let's break down the problem step-by-step:
---
## **Step 1: Write the Electrical Equation**
The armature circuit is described by:
\[
e_{in}(t) = R I_L(t) + \frac{d\lambda}{dt}
\]
where:
- \( e_{in}(t) \) = input voltage
- \( R \) = resistance
- \( I_L(t) \) = solenoid current
- \( \lambda \) = magnetic flux linkage
From the problem:
\[
I_L(\lambda) = a_3 \lambda^3 + a_1 \lambda
\]
So,
\[
I_L(t) = a_3 \lambda^3(t) + a_1 \lambda(t)
\]
---
## **Step 2: Write the Mechanical Equation (Newton's Second Law)**
The forces on the mass \( m \) are:
- Electromagnetic force: \( F_{em}(\lambda) \)
- Spring force: \( -kx \)
- Damping force: \( -b\dot{x} \)
- Inertia: \( m\ddot{x} \)
So,
\[
m\ddot{x} + b\dot{x} + kx = F_{em}(\lambda)
\]
From the problem:
\[
F_{em}(\lambda) = c_6 \lambda^6 + c_4 \lambda^4 + c_2 \lambda^2
\]
---
## **Step 3: Complete Mathematical Model**
Combine all equations:
### **Electrical Subsystem:**
\[
e_{in}(t) = R I_L(t) + \frac{d\lambda}{dt}
\]
with
\[
I_L(t) = a_3 \lambda^3(t) + a_1 \lambda(t)
\]
### **Mechanical Subsystem:**
\[
m\ddot{x} + b\dot{x} + kx = c_6 \lambda^6 + c_4 \lambda^4 + c_2 \lambda^2
\]
---
## **Step 4: Coupling Between Electrical and Mechanical Systems**
The flux linkage \(\lambda\) depends on the position \(x\), but the problem does not provide a direct relationship here. If needed, the coupling would be provided as \(\lambda = \lambda(x, I_L)\), but for this problem, \(\lambda\) is treated as an independent variable.
Assume the spring is at equilibrium ( \( x = 0 \) ) when \( F_{em} = 0 \).
---
## **Step 5: Final Model Summary**
### **1. Electrical Equation:**
\[
e_{in}(t) = R [a_3 \lambda^3(t) + a_1 \lambda(t)] + \frac{d\lambda}{dt}
\]
### **2. Mechanical Equation:**
\[
m\ddot{x}(t) + b\dot{x}(t) + kx(t) = c_6 \lambda^6(t) + c_4 \lambda^4(t) + c_2 \lambda^2(t)
\]
where \( \lambda \) is the magnetic flux linkage (state variable), and \( x \) is the displacement of the armature mass.
---
## **Final Answer (Boxed):**
\[
\boxed{
\begin{align*}
&\text{Electrical:} \quad e_{in}(t) = R [a_3 \lambda^3(t) + a_1 \lambda(t)] + \frac{d\lambda}{dt} \\
&\text{Mechanical:} \quad m\ddot{x}(t) + b\dot{x}(t) + kx(t) = c_6 \lambda^6(t) + c_4 \lambda^4(t) + c_2 \lambda^2(t)
\end{align*}
}
\]
This is the **complete mathematical model** of the electromechanical actuator as described in the problem.
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