>
Course Unit Title Course Unit Code Type of Course Unit Level of Course Unit Year of Study Semester ECTS Credits
Electronics Instruments and Systems UGM207 Compulsory Bachelor's degree 2 Fall 4

Name of Lecturer(s)

Associate Prof. Dr. Satılmış ÜRGÜN
Lecturer Nezih KAYA

Learning Outcomes of the Course Unit

1) Describes typical system arrangements of electronic instrument systems and their cockpit layout
2) Explain operation principles and structure of the data buses in the aircraft.
3) Explain structure and role of fiber-optics in data communication in the aircraft.
4) Explain the forming conditions and problems about static electricity.
5) Explain the concept of electromagnetic interference and its effects.
6) Explains software management control in aviation
7) Explain the operation of typical Electronic / Digital Aircraft Systems and their relationship with each other.
8) Explain the types of electronic displays and their operations.

Program Competencies-Learning Outcomes Relation

  Program Competencies
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19
Learning Outcomes
1 Middle Low Low Low High Low High High Low High Low Middle High Low High High Low High High
2 High Middle Low Middle Middle Low Middle High Low Middle Low Middle Middle Low Low Low Low Low Low
3 High Middle Low Low Middle Low Middle Middle Low Middle Low Middle High Low Middle Middle Middle Middle Low
4 High Low Low Middle Low Middle Low Low High Low Low Low High Low Low Low High Low Low
5 Middle Middle Low Low Middle Low High High High Low Low Middle Middle Low High High High Middle High
6 Middle Low Low Low High Low Middle Middle Low Low Low Middle High Low High Middle Low Middle Middle
7 Middle Middle Low High High Low High High Low High Low Low High Low High Middle Low Middle High
8 Middle Middle Middle Middle Low Middle Middle Low Middle Low Low Middle Low Middle Middle Low Middle Low Middle

Mode of Delivery

Face to Face

Prerequisites and Co-Requisites

None

Recommended Optional Programme Components

Not Required

Course Contents

Typical systems arrangements and cockpit layout of electronic instrument systems. Fiber Optics; Advantages and disadvantages of fibre optic data transmission over electrical wire propagation; Fibre optic data bus; Fibre optic related terms; Terminations;Couplers, control terminals, remote terminals; Application of fibre 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-static protection devices. Software Management, Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programmes. 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 digital aircraft systems; General arrangement of typical electronic/digital aircraft systems and associated BITE (Built In Test Equipment) such as: ACARS-ARINC Communication and Addressing and Reporting System EICAS-Engine Indication and Crew Alerting System, FBW-Fly-by-Wire, FMS-Flight Management System, IRS-Inertial Reference System; ECAM-Electronic Centralised Aircraft Monitoring, EFIS-Electronic Flight Instrument System, GPS-Global Positioning System, TCAS-Traffic Alert Collision Avoidance System, Integrated Modular Avionics, Cabin Systems, Information Systems

Weekly Schedule

1) Typical systems arrangements and cockpit layout of electronic instrument systems. Fiber Optics;
2) Fiber Optics; Advantages and disadvantages of fibre optic data transmission over electrical wire propagation; Fibre optic data bus; Fibre optic related terms; Terminations;Couplers, control terminals, remote terminals; Application of fibre optics in aircraft systems
3) 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.
4) Electrostatic sensitive devices; Special handling of components sensitive to electrostatic discharges; Awareness of risks and possible damage, component and personnel anti-static protection devices.
5) EMC-Electromagnetic Compatibility; EMI-Electromagnetic Interference, HIRF-High Intensity Radiated Field, Lightning/lightning protection
6) Software Management, Awareness of restrictions, airworthiness requirements and possible catastrophic effects of unapproved changes to software programmes
7) Typical digital aircraft systems; General arrangement of typical electronic/digital aircraft systems and associated BITE (Built In Test Equipment) such as: ACARS-ARINC Communication and Addressing and Reporting System
8) EICAS-Engine Indication and Crew Alerting System, ECAM-Electronic Centralised Aircraft Monitoring, EFIS-Electronic Flight Instrument System,
9) FBW-Fly-by-Wire,
10) FMS-Flight Management System,
11) IRS - Inertial Navigation/Referans System GPS - Global Positioning System TCAS : Traffic Collision Avoidance System
12) Integrated Modular Avionics
13) Cabin Systems,
14) Information Systems
15) Final Exam week
16) Final exam

Recommended or Required Reading

Planned Learning Activities and Teaching Methods

1) Lecture
2) Question-Answer
3) Discussion
4) Demonstration
5) Self Study


Assessment Methods and Criteria

Contribution of Midterm Examination to Course Grade

50%

Contribution of Final Examination to Course Grade

50%

Total

100%

Language of Instruction

Turkish

Work Placement(s)

Not Required