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Department of Aeronautical Engineering, REC



              Subject Code                         Subject Name                          Category   L  T  P  C
               AV19P217               AIRBORNE ACTUATORS AND SENSORS                        PE      3  0  0  3


             Objectives:
              ⚫   To learn the concept of actuation systems, its types and servo components.
              ⚫   To study modeling, design and testing of aircraft actuation systems.
              ⚫   To understand the principles of gyroscope, gyro equation and test methodologies.
              ⚫   To learn the concept of sensor testing.
              ⚫   To introduce various types of aircraft actuation systems, inertial sensors, modelling and testing of sensors.

             UNIT-I     AIRCRAFT ACTUATION SYSTEMS                                                       9
             Introduction -Principles of actuation systems, Types of actuation systems.
             UNIT-II    SERVO COMPONENTS                                                                 9
             Actuators, Valves, Servo amplifiers pick-offs.
             UNIT-III   MODELING, DESIGN, AND TESTING                                                    9
             Linear and non-linear actuation system, modeling of actuation systems, Servo-loop analysis actuator design - testing
             methodologies, Performance testing test equipments for actuation systems.
             UNIT-IV    INERTIAL SENSORS                                                                 9
             Gyroscope- Principles , Gyro equations, Rate Gyros - Rate integration and free Gyro, Vertical and Directional Gyros,
             Laser  Gyroscopes  -  Inertial  navigation  -  Basic  principles,  theory  and  applications.  Accelerometers--  Principles  &
             Theory, Spring mass, force balance and piezo-electric accelerometers, MEMS sensors
             UNIT-V     SENSOR TESTING                                                                   9
             Test philosophies and methodologies, Test equipment, Performance testing of sensors.
                                                                                 Total Contact Hours   :   45

             Course Outcomes:
             On completion of the course students will be able to
                 Students will explain the advanced concepts in Active Control Technology to the engineers and provide the
              ⚫
                 necessary mathematical knowledge that is needed in modeling physical processes.
              ⚫   Explain the principle of actuation system, types of actuation system, servo valves and servo amplifiers pick-offs.
              ⚫   Perform design and testing on actuation systems and sensors.
              ⚫   Discuss the principle, theory and application of inertial sensors.
                 Get exposure on various topics such as aircraft actuation systems, servo-components, inertial sensors, modeling,
              ⚫   design and testing of sensors and will be able to deploy these skills effectively in the solution of problems in
                 avionics engineering.

             Text Books:
                 James Ephraim Johnson, Electro-hydraulic Servo Systems, Published by Editors of Hydraulics & pneumatics
              1
                 magazine, 1977.
              2   Neal E.Wood et al, ‘Electro-mechanical actuation development AFFDL-TR-150’ DEC 1978.

             Reference Books / Web links:
              1   Pallett, E.H.J. ‘Aircraft instruments, principles and applications’, Pitman publishing Ltd., London, 1981.


















            Curriculum and Syllabus | M.E. Avionics | R2019                                           Page 52
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