INTRODUCTION
In the DC servomotor that includes two windings; a stationary field winding on the stator and a second winding for the rotating armature. This type of motor can be controlled by varying either the field current or the armature current. Most modern servomotors are somewhat different in construction. The field winding is replaced with two or more powerful rareearth magnets on the stator. Since the field strength of these motors is constant, they can only be controlled by varying the armature current, in a permanent magnet motor the output torque, is directly proportional to the armature current, The constant of proportionality is referred to as the torque constant of the motor and is represented . The transfer function relating motor torque to armature current can be expressed as follows: DC servomotor that includes two windings; a stationary field winding on the stator and a second winding for the rotating armature. This type of motor can be controlled by varying either the field current or the armature current. Most modern servomotors are somewhat different in construction. The field winding is replaced with two or more powerful rareearth magnets on the stator. Since the field strength of these motors is constant, they can only be controlled by varying the armature current, In a permanent magnet motor the output torque, is directly proportional to the armature current, The constant of proportionality is referred to as the torque constant of the motor and is represented The transfer function relating motor torque to armature current can be expressed as follows:
ABOUT OUR TRAINER
Pictorial View
Front Panel View
Specification
Armature voltage Va

0  50V DC

Field Voltage Vf

0  50VDC

AC voltage

0 – 20 VAC.

Armature winding voltage

50V DC

Field winding voltage

50V DC

Power

120W

Armature current (Ia)

2.6A(max)

Moment of inertia (J)

g/cm2.

Front Panel Description
DC voltmeter

DC Ammeter

AC voltmeter

AC Ammetera

Armature volt adjustment
Pot = Adjust the armature voltage from 3V to 50V.

Pot = Adjust the armature voltage from 3V to 50V.

A and AA = Connect to the motor armature terminal respectively.

Field Volt Adjustment
Pot = Adjust the field voltage from 0V to 50V.

Switch ‘S2' = Switch ON/OFF the field voltage.

F and FF = Connect to the motor field terminal respectively.

AC voltage = Adjust the AC voltage from 0V to 20V.

AC output (P&N) = AC output voltage.

Principle of Operating
A DC servomotor is used in a control system where an appreciable amount of shaft power is required. The DC servomotor are either armaturecontrolled with fixed field, or fieldcontrolled with fixed armature current. DC servomotor used in instrument employ a fixed permanentmagnet field, and the control signal is applied to the armature terminals.
T_{m} = K_{m}Φ_{f}i_{a}  (i)
Km = Proportionality constant
Tm = Motor torque Nf = Field flux ia = Armature current
In addition to the torque when conductor moves in magnetic field, voltage is generated across its terminals which opposes the current flow and hence called as Back e.m.f denoted as eb
e_{b}= K_{m}Φω_{m} (ii)
This back e.m.f is directly proportional to the shaft velocity Tm. Equations (i) and (ii) form the basic equation of d.c. servo motor operation.
Basic Classification
Basically d.c. servo motors are classified as:
☞Variable magnetic flux motors.
☞Constant magnetic flux motors.
In variable magnetic flux motors magnetic field is produced by the field windings which are connected to the external supply. These are also called as separately excited or field controlled motors.
The constant magnetic flux motors are also known as permanent magnet d.c. motors. These motors have relatively linear torquespeed characteristics.
Derivation of transfer functions for
☞Field controlled d.c. servo motor
☞Armature controlled d.c. servomotors.
Assumptions
(1) Constant armature current is fed into the motor.
(2) Nf % If. Flux produced is proportional to field current. Nf = Kf If
(3) Torque is proportional to product of flux and armature current.
Tm % N Ia . Tm = K` N Ia = K’ Kf If Ia Tm = Km Kf If
Where
Km = K`
Ia = constant
Apply kirchoff’s law to field circuit.
L _{f}di_{f} / dt + R_{f} I_{f} = e_{f}
Now shaft torque Tm is used for driving load against the inertia and frictional torque.
Finding Laplace Transforms of equations (1), (2) and (3) we get,
Tm (s) = Km Kf If(s) Ef (s) = (SLf + Rf) If (s) Tm (s) = Jms 2m (s) + Bms2m (s)
Eliminate If (s) from equations (4) and (5)Input = Ef(S)
Output = Rotational displacement 2m (S)
Armature Controlled D.C. Servo Motor
Assumptions
(i) Flux is directly proportional to current through field winding.
Nm = Kf If = constant
(ii) Torque produced is proportional to product of flux and armature current.
T = K`m N Ia T = K`m Kf If Ia
(iii) Back e.m.f is directly proportional to shaft velocity Tm, as flux N is constant.
as ω_{n} = dθ(t) / dt
E_{b} = k_{b}ω_{m}(d) = K_{b}sθ_{m}(s)
Apply Kirchhoff’s law to armature circuit:
Where Jm = Jm/Bm and
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