RAE501 AIS Syllabus
AKTU Aeronautical Engineering(AE) RAE501AIS Syllabus for all 5 units are provided below. Download link for AE 5th SEM RAE501 Aircraft Instruments &System Syllabus is listed down for students to make perfect utilization and score maximum marks with our study materials.
UP Technical University Aeronautical Engineering(AE) 5th SEM RAE501 AIS – Aircraft Instruments &System Syllabus
RAE 501: AIRCRAFT INSTRUMENTS& SYSTEMS
UNIT-1
Electronic Instrument System: Typical system arrangement and cockpit layout of Electronics
instrument systems. Numbering System: binary, octal and hexadecimal: Demonstration of
conversion between the decimal And binary, octal and hexadecimal systems and vice versa.
Logic Circuits: Identification of common logic gate symbols and equivalent circuits.
Application used for aircraft systems.
UNIT-2
Data Conversion: Analogue Data, Digital Data: Operation and application of analogue to
digital, and digital to analogue converters, inputs and outputs, limitations of various types Data
Buses: Operation of data buses in aircraft systems, including knowledge of ARINC and other
specifications. schematic diagrams. Interpretation of logic diagrams.
UNIT-3
Microprocessors: Functions performed and overall operation of a microprocessor. Basic
operation of each of the following microprocessor elements: control and processing unit, clock,
register, arithmetic logic unit. Integrated Circuits, Operation and use of encoders and decoders;
Function of encoder types; Uses of medium, large and very large scale integration. Multiplexing.
Operation, application and identification in logic diagrams of multiplexers and DE multiplexers.
UNIT-4
Fiber Optics: Advantages and disadvantages of fiber optic data transmission over electrical wire
propagation: Fiber optic data bus, Fiber optic related terms, Termination, Couplers, control
terminals, remote terminals. Application of fiber optics in aircraft systems.
Electronic Displays: Principles of operation of common types of displays used in modern
aircraft, including Cathode Ray Tubes, Light Emitting Diodes and Liquid Crystal Display.
Electrostatic Sensitive Devices. Special handling of components sensitive to electrostatic
discharges. Awareness of risks and possible damage, component and personnel anti-state
protection devices. Software Management Control.
UNIT-5
Electromagnetic Environment: Influence of the following phenomena on maintenance
practices for electronic system: EMC-Electromagnetic Compatibility EMI Electromagnetic
Interference HIRF-High Intensity, Radiated Field. Lightning, lightning protection. Typical
Electronic/Digital Aircraft Systems. General arrangement of typical electronics.
Digital aircraft system and associated BTTE(Built in Test Equipment): Testing such as:
ACARS-ARINC Communication and Addressing and Reporting System, ECAM- Electronics.
Centralized Aircraft Monitoring. EFIS- Electronics Flight Instrument System, EICAS- Engine
Indication and Crew Alerting System, FBW-Fly by Wire, FMS- Flight Management System,
GPS- Global Positioning System & IRS-Inertial Reference System.
Books and References:
1. Pallet, E.H.J, “Aircraft Instruments & Principles”, Pitman & Co 1993.
2. Casamassa, J.V., and Bent R., Jet Aircraft Power Systems, McGraw Hill Book Co., New
York,1975
3. Bent, R.D. Mickinely., Aircraft Maintenance and Repair, 2nd Edition – McGraw Hill Inc
., NowYork, 1978.
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RAE501 Syllabus, AIS Unit-wise Syllabus – AE 5th Semester
