Practice Problems (KEY)#

Problem 1.#

An inertial navigation system’s (INS) accelerometers put out \(-70\ \text{mV}\) when \(-5g\) is detected and \(20\ \text{mV}\) when \(5g\) is detected. An aircraft’s navigation system reads voltages between \(-7\ \text{V}\) and \(2\ \text{V}\) when the detected signal is between \(-5g\) and \(5g\). Design a signal conditioning circuit to adjust the INS to the nav system.

Step 1 — Linear Model#

\[ V_{\text{out}} = K V_{\text{in}} + B \]

Step 2 — Write Two Equations#

At \(-5g\):

\[ (-70\ \text{mV})K + B = -7\ \text{V} \]

At \(5g\):

\[ (20\ \text{mV})K + B = 2\ \text{V} \]

Step 3 — Eliminate \(B\)#

\[ (140\ \text{mV})K = 14\ \text{V} \]
\[ K = 100 \]

Step 4 — Solve for \(B\)#

\[ (-70\ \text{mV})(100) + B = -7\ \text{V} \]
\[ -7\ \text{V} + B = -7\ \text{V} \]
\[ B = 0 \]

Final System: Amplifier only with \(K = 100\).


Problem 2.#

An elevator for a UAS requires \(1\ \text{V}\) to move the elevator fully down and \(-9\ \text{V}\) to move the elevator fully up. The pilot’s control column (joystick) produces \(-1\ \text{mV}\) when fully down and \(4\ \text{mV}\) when fully up. Design the interface between the control unit and the actuator.

Linear Model#

\[ V_{\text{out}} = K V_{\text{in}} + B \]

Write Two Equations#

\[ (-1\ \text{mV})K + B = 1\ \text{V} \]
\[ (4\ \text{mV})K + B = -9\ \text{V} \]

Eliminate \(B\)#

\[ (5\ \text{mV})K = -10\ \text{V} \]
\[ K = -2000 \]

Solve for \(B\)#

\[ (-1\ \text{mV})(-2000) + B = 1\ \text{V} \]
\[ 2\ \text{V} + B = 1\ \text{V} \]
\[ B = -1\ \text{V} \]

Final System: Amplifier and summer required.


Problem 3.#

For each of the following devices, determine whether it is an input transducer, an output transducer, both, or neither.

a. Computer mouse — Input transducer. Converts physical motion into an electrical signal.

b. Electric motor — Output transducer. Converts electrical energy into mechanical motion.

c. Stereo speakers — Output transducer. Convert electrical signals into sound.

d. Op amp — Neither. It amplifies electrical signals but does not interact directly with the physical world.

e. Light bulb — Output transducer. Converts electrical energy into light.

f. Electronic thermometer — Input transducer. Converts temperature into an electrical signal.

g. Transformer — Neither. Converts one electrical signal to another electrical signal.

h. iPhone touch screen — Both. Detects touch (input) and displays information (output).

i. Control stick of a fly-by-wire aircraft — Input transducer. Converts mechanical displacement into an electrical signal.

j. Aircraft HUD (Head Up Display) — Output transducer. Converts electrical signals into visual information.


Problem 4.#

Why don’t we use transformers to amplify information signals?

There are two primary reasons:

  1. Transformers conserve power. If voltage increases, current decreases proportionally. True amplification requires increasing power, not simply trading voltage for current.

  2. Transformers require AC signals. Information signals that change slowly or contain DC components will not pass properly through a transformer.


Problem 5.#

A device that is used to add two or more signals is a

a. Input transducer
b. Output transducer
c. Summer
d. Instrumentation System

Correct Answer: c. Summer


Problem 6.#

A microphone converts an incoming voice signal to a range of \(\pm 2.5\ \text{mV}\). Design an instrumentation system to amplify this signal to drive a speaker which requires \(\pm 4\ \text{V}\).

Since both input and output are symmetric about zero:

\[ B = 0 \]
\[ K(2.5\ \text{mV}) = 4\ \text{V} \]
\[ K = 1600 \]

Final System: Amplifier with gain \(1600\).


Problem 7.#

Using the instrumentation system you designed in Problem 6 above, what would the output voltage be if the signal from the microphone was \(1\ \text{mV}\)?

\[ V_{\text{out}} = K V_{\text{in}} \]
\[ V_{\text{out}} = (1600)(1\ \text{mV}) = 1.6\ \text{V} \]

Problem 8.#

The rudder control unit for a fly-by-wire aircraft produces a \(-2.5\ \text{mV}\) signal when fully left is desired and \(2.5\ \text{mV}\) for fully right. The rudder actuator requires \(-5\ \text{V}\) for fully left and \(+10\ \text{V}\) for fully right.

Linear Model#

\[ V_{\text{out}} = K V_{\text{in}} + B \]

Two Equations#

\[ (2.5\ \text{mV})K + B = 10\ \text{V} \]
\[ (-2.5\ \text{mV})K + B = -5\ \text{V} \]

Eliminate \(B\)#

\[ (5\ \text{mV})K = 15\ \text{V} \]
\[ K = 3000 \]

Solve for \(B\)#

\[ (2.5\ \text{mV})(3000) + B = 10\ \text{V} \]
\[ 7.5\ \text{V} + B = 10\ \text{V} \]
\[ B = 2.5\ \text{V} \]

Final System: Amplifier and summer required.


Problem 9.#

The flight control computer generates a \(4\ \text{mV}\) signal when the ailerons need to be deflected \(15^\circ\) and a \(-16\ \text{mV}\) signal when \(-20^\circ\) deflection is needed. The aileron actuators require \(15\ \text{V}\) and \(-10\ \text{V}\) respectively.

Linear Model#

\[ V_{\text{out}} = K V_{\text{in}} + B \]

Two Equations#

\[ (4\ \text{mV})K + B = 15\ \text{V} \]
\[ (-16\ \text{mV})K + B = -10\ \text{V} \]

Eliminate \(B\)#

\[ (20\ \text{mV})K = 25\ \text{V} \]
\[ K = 1250 \]

Solve for \(B\)#

\[ (4\ \text{mV})(1250) + B = 15\ \text{V} \]
\[ 5\ \text{V} + B = 15\ \text{V} \]
\[ B = 10\ \text{V} \]

Final System: Amplifier and summer required.