Aircraft Systems and Controls detailed Syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUH official website and presented for the students affiliated to JNTUH course structure. For Course Code, Subject Names, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the universities official website.
For all other AERO 3rd Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH, do visit AERO 3rd Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH Subjects. The detailed Syllabus for aircraft systems and controls is as follows.
Pre-requisite:
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Course Objectives:
- Explain the concept and meaning of system and classify the various systems required for aircraft and their contribution in order to fulfil the aircraft tasks.
- Describe the various types of Electrical power generations and distribution in aircraft.
- Impart the knowledge of pneumatic, hydraulic and environmental control system.
- Demonstrate different actuators, flight control system and advanced flight actuation system.
Course Outcomes:
- The principles of flight control
- The principle and working of electronic and mechanical control systems
- Various types of aircraft instruments
- Static and dynamic characteristics of instruments
Unit I
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Unit II
Electrical Systems and Air Conditioning, Pressurizing Systems: Electrical loads in aircraft. Electrical power generation and control- DC, AC- types. Power distribution- primary, secondary. Power conversion and energy storage; Load protection; Electrical load management systems, variable speed constant frequency (VSCS) cycloconverter, 270 V DC systems; Basic air cycle systems; Vapour cycle systems, boost-strap air cycle system; Evaporative vapour cycle systems; Evaporative air cycle systems; Oxygen systems; Fire protection systems, de-icing and anti icing systems.
Unit III
Hydraulic Systems and Pneumatic Systems: Hydraulic systems: Study of typical workable system, function, merits, application, system loads, design requirements; Principal components; Hydraulic fluid: required properties, operating fluid pressures, temperatures, and flow rates; Hydraulic piping, pumps, reservoir, accumulator; Landing gear and brake management systems. Pneumatic systems; Advantages; – Working principles; Typical air pressure system; Brake system; Typical pneumatic power system; Components, landing gear systems; Classification.
Unit IV
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Unit V
Airplane Control Systems: Flight control systems- primary and secondary flight control conventional systems; Power assisted and fully powered flight controls ; Power actuated systems; Engine control systems; Push pull rod system, flexible push full rod system; Components; Modern control systems; Digital fly by wire systems , control laws, implementation; Auto pilot system active control technology, communication and navigation systems instrument landing systems; Control linkages, actuation- types, description and redundancy.
Text Books:
- Moir, I. and Sea bridge, A, Aircraft Systems: Mechanical, Electrical and Avionics Subsystems Integration!, John Wiley, 3rd Edition 2008.
- Moir, I. and Sea bridge, A, Design and Development of Aircraft Systems- An Introduction!, AIAA Education Series!, AIAA, 2004.
Reference Book:
For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
For detail Syllabus of all other subjects of B.Tech 3rd Year Aeronautical Engineering, visit AERO 3rd Year Syllabus Subjects.
For all B.Tech results, visit JNTUH B.Tech all years, and semester results from direct links.