Subject description - AE0B38LPT

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AE0B38LPT Aircraft Instrumentation
Roles:V Extent of teaching:2P+2L
Department:13138 Language of teaching:EN
Guarantors:  Completion:Z,ZK
Lecturers:  Credits:5
Tutors:  Semester:L


The course deals with theory and description of function of aircraft's low frequency instruments and systems. Students test them and measure their parameters in laboratory courses.

Course outlines:

1. Airborne instruments; basic overview; purpose and use, cockpit equipment,
alignment according to the aircraft
2. Engine parameters, overview, and units. Revolution measurement of
turbojet and propeller engines.
3. Cylinder head and exhaust gas temperature measurement. Anti-ice systems.
Fire annunciators.
4. Torque, fuel used and fuel flow and engine vibration measurement.
5. Complex system for engine parameters measurement.
6. Fuel system, measurement of total and critical amount of fuel.
7. Barometrical and inertial measurement of altitude. Altimeters and their
types. Standard atmosphere.
8. Aerometrical flight measurement, theory, Speedometer construction
9. Vertical speed measurement, mach-number measurement, machmeters and
variometer construction.
10. Aerometric data computer, process of data calculation, aerometrical
11. Mechanical gyroscopes. Gyro-horizon, correction system. Rate-of-turn
12. Magnetic compass. Gyro-magnetic compass; principles of operation and
13. Inertial navigation systems; principles of operation. Strapdown inertial
system; structure and description.
14. Central flight, navigation and monitoring airborne systems.

Exercises outline:

1. Revolution indicator measurement
2. Exhaust-gas temperature indicator check
3. Check of the system for torque measurement
4. Measurement of parameters of the fuel pressure sensor and oil pressure
5. Fuel consumption indicator check
6. Altimeter indicator calibration using PC system
7. Speed indicator calibration using PC system
8. Check of the airborne variometer
9. Measurement of precessional drift of the gyroscope
10. Evaluation of the gyroscope drift during simulated axis movement
11. Measurement of parameters of the gyroscope rate-of-turn indicator
12. Gyro-horizon parameter measurement and function demonstration
13. Gyro-magnetic compass check
14. Simulation of central monitoring aircraft system by PC


1. Michael H. Tooley: Aircraft Digital Electronic and Computer Systems:
Principles, Operation and Maintenance. Butterworth-Heinemann (11 Dec 2007) ISBN-10: 0750681381



Subject is included into these academic programs:

Program Branch Role Recommended semester
BEKME1 Communication Technology V
BEKME5 Komunikace a elektronika V
BEKME_BO Common courses V
BEKME4 Network and Information Technology V
BEKME3 Applied Electronics V
BEKME2 Multimedia Technology V
BEEEM1 Applied Electrical Engineering V
BEEEM_BO Common courses V
BEEEM2 Electrical Engineering and Management V
BEKYR1 Robotics V
BEKYR_BO Common courses V
BEKYR3 Systems and Control V
BEKYR2 Sensors and Instrumentation V
BEOI1 Computer Systems V
BEOI_BO Common courses V
BEOI3 Software Systems V
BEOI2 Computer and Information Science V

Page updated 22.6.2021 19:54:31, semester: L/2021-2, L/2020-1, Z,L/2022-3, Z/2021-2, Send comments about the content to the Administrators of the Academic Programs Proposal and Realization: I. Halaška (K336), J. Novák (K336)