INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

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INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, yderabad - 500 043 AERONAUTICAL ENGINEERING COURSE DESCRIPTION FORM Course Title Course Code Regulation Course Structure Course Coordinator Team of Instructors AVIONICS AND INSTRUMENTS SYSTEMS A82129 R13 - JNTU Lectures Tutorials Practical s Credits 4 - - 4 Mr. P. Anudeep, Assistant Professor, Department of Aeronautical Engineering. Mr. P. Anudeep, Assistant Professor, Ms. M. Mary Thraza, Assistant Professor, Mr. Naresh Eppakayala, Assistant Professor, Department of Aeronautical Engineering. I. COURSE OVERVIEW The Avionics and Instruments course will enable the student to enhance his/her knowledge in the field of the instruments, sensors, communication techniques, and other equipment used onboard an aircraft. The course cover in detail about the evolution of the aviation electronics and moves further and discusses the important topics like navigation, communication, sensors and displays implemented in a civil aviation, later the military adaptation of the same will be discussed. The course will be discussing the topics like RADAR, GPS etc. which impart a thorough understanding of these modern-day technologies. The course will make the student realize the importance of electronics in the working of an aircraft. II. PREREQUISITE(S) Level Credits Periods / Week Prerequisite UG 4 5 Aircraft Systems, Electrical and Electronics Engineering III. MARKS DISTRIBUTION Mid Semester Test Session Marks There shall be two midterm examinations. Each midterm examination consists of essay paper, objective paper,and assignment. The essay paper is for 10 marks of 60 minutes duration and shall contain 4 questions. The student has to answer 2 questions, each carrying 5 marks. The objective paper is for 10 marks of 20 minutes duration. It consists of 10 multiple choice and 10 fill-in-the-blank questions, the student has to answer all the questions and each carries half mark. The first midterm examination shall be conducted for the first two and a half units of syllabus and second midterm examination shall be conducted for the remaining portion. Assignment University End Exam Marks Total Marks 75 100

Five marks are marked for assignments. There shall be two assignments in every theory course. Assignments are usually issued at the time of commencement of the semester. These are of problem-solving in nature with critical thinking. Marks shall be awarded considering the average of two midterm tests in each course. IV. EVALUATION SCEME S No Component Duration Marks 1 I Mid examination 80 minutes 20 2 I Assignment -- 05 3 II Mid examination 80 minutes 20 4 II Assignment -- 05 5 External examination 3 hours 75 V. COURSE OBJECTIVES: VI. The course enables the students to: I. Understand the core avionics concept in aircrafts. II. Describes the Avionics classification based on theelectromagnetic spectrum. III. Impart the knowledge of Communication, Navigation and Surveillance for Aircrafts. IV. Illustrates the application of Avionics in Flight controlling V. Impart the knowledge of Avionics used in Military aircrafts. COURSE OUTCOMES At the end of the course the students are able to: 1. Describe the basic principles of operation of the avionics and their sub- that make up a typical integrated system. 2. Illustrate the Flight manage with controls and displays. 3. Describe the information required and generated by the sub- of avionics 4. Categorize requirement of the avionics and subsystem for military aircrafts. 5. Explain the basic operation of automatic flight control. 6. Discuss the functionalities of radars & antennas and their types for spacecraft applications. 7. Explain the operation of magnetic navigation equipment. 8. Analyze and discuss the baseline design-stability & control, performance,and constraint analysis. 9. Describe the terrain awareness and Traffic collision avoidance system. 10. Describe the system requirements for flight data recorders (FDR). VII. OW PROGRAM OUTCOMES AREASSESSED PO1 PO2 PO3 PO4 Program outcomes Engineering knowledge: Knowledge in fundamentals of mathematics, science,and engineering. Problem analysis: An ability to identify, formulate and solve problems in key areas of Aerodynamics, Structures, Propulsion, Flight Dynamics and Control, Design, Testing, Space and Missile Technologies and Aviation of Aeronautical Engineering discipline. Design/development of solutions: An ability to design and conduct experiments, analyze and interpret data related to various areas of Aeronautical Engineering. Conduct investigations of complex problems: An ability in conducting investigations to solve problems using research-based knowledge and methods to Level S Proficiency assessed by Assignments Lectures, Assignments Lectures, Tutorials Lectures

PO5 PO6 PO7 provide logical conclusions. Modern tool usage: Skills to use modern engineering and IT tools, software and equipment to analyze the problems in Aeronautical Engineering. The engineer and society: Understanding of theimpact of engineering solutions on the society to assess health, safety, legal, and social issues in Aeronautical Engineering. Environment and sustainability: The impact of professional engineering solutions in anenvironmental context and to be able to respond effectively to the needs of sustainable development. Lectures, Tutorials PO8 Ethics: The knowledge of Professional and ethical responsibilities. PO9 PO10 PO11 PO12 Individual and teamwork: An ability to work effectively as an individual and as a team member/leader in multidisciplinary areas. S Discussions Communication: An ability to critique writing samples (abstract, executive summary, project report), and oral presentations. Project management and finance: The need forself-education and ability to engage in lifelong learning. Seminars Life-long learning: Knowledge of management principles and apply these to manage projects in multidisciplinary environments. Guest lectures S Supportive ighly Related VIII. OW PROGRAM SPECIFIC OUTCOMES ARE ASSESSED PSO1 PSO2 PSO3 PSO4 Program Specific Outcomes Level Professional skills: Able to utilize the knowledge of aeronautical/aerospace engineering in theinnovative, dynamic and challenging environment for design and S development of new products. Problem-solving skills: Imparted through simulation language skills and general purpose CAE packages to solve practical, design and analysis problems of components to complete the challenge of airworthiness for flight vehicles. Practical implementation and testing skills: Providing different types of in-house and training and industry practice to fabricate and test and develop the products with more innovative technologies. Successful career and entrepreneurship: To prepare the students with thebroad aerospace knowledge to design and develop and sub of aerospace S and allied and become technocrats. S Supportive ighly Related Proficiency assessed by Seminars Guest Lectures IX. SYLLABUS UNIT-I: AVIONICS INTRODUCTION-AVIONICS STANDARDS Importance and role of avionics in modern aircraft-core avionics and interface with pilot-aircraft state sensor, outside world sensor -task automation. Requirements of avionics equipment and environmental, weight, reliability Standardization and specifications of avionics equipment and -the ARNC and MIL specifications. Electrical and optical data bus -integrated modular avionics architectures-avionics packaging. UNIT-II: DISPLAYS-MAN MACINE INTERACTION AND COMMUNICATION SYSTEMS Introduction to aircraft displays head up displays (UD)-basic principles. elmet mounted displays, head tracking. ead down displays-civil cockpit, military cockpit.solid state standby display. Data fusion in displays-intelligent display management

Introduction to voice and data communication -F, VF, UF and satellite communications-data recorders- Audio management -in-flight entertainment -ACARS data communication. UNIT-III: INERTIAL SENSORS AND GLOBAL POSITIONING SYSTEMS Basic principles of gyroscopes and accelerometers-angular momentum gyros-dynamically tuned gyro-micro machined vibrating mass rate gyro.introduction to optical gyroscopes-ring laser gyros-principles. Specific force measurements with accelerometers, torque balance pendulous accelerometers. Stable platform -strap down -errors in inertial and compensations. Global Navigational satellite -the global positioning system (GPS)-description and basic principlesintegration of GPS and INS-differential GPS augmented satellite navigation. UNIT-IV: NAVIGATION RANGING AND LANDING SYSTEMS Introduction and Basic principles of navigation-types of navigation - Radio-navigation -VF Omnirange, distance measuring equipment, automatic direction finders.attitude and heading reference. Inertial Navigation (INS)-platform axes angular rate corrections, acceleration correction, initial alignment and gyro-compassingstrap-down INS computing. Aided INS-Kalman filters. Landing -localizer and glide slope-marker. Categories of instrument landing. UNIT-V: SURVEILLANCE SYSTEMS AND AUTOFLIGT SYSTEMS Traffic alert and collision avoidance (TCAS)-Enhanced ground proximity warning -Air traffic control -Mode S transponders-predictive wind shear warning -weather radar -Enhanced ground proximity warning Longitudinal and lateral control and response of aircraft-powered flight controls-auto-stabilization. Autopilots-principles-height control-heading control-ils coupled autopilot control-automatic landing satellite landing guidance -speed control and autothrottle control. Flight management principles-flight planning-navigation and guidance-flight path optimization and performance prediction-cost index. TEXTBOOK 1. Collinson,R.P.G.,IntroductiontoAvionicsSystems,secondedition,Springer,2003,ISBN978-81-8489-795-1 2. Moir, I. and Sea bridge, A., Civil Avionics Systems, AIAA Education Series, AIAA, 2002, ISBN 1-56347589-8. 3. Moir, I., Sea bridge, A. & Jukes, M., Military Avionics Systems (Aerospace), Wiley, 2006, ISBN-10: 0470016329, ISBN-13: 9780470016329 REFERENCES 1. Kayton, M., & Fried, W.R., Avionics Navigation Systems, Wiley, 1997, ISBN 0-471-54795-6. 2. elfrick, A., Principles of Avionics, Avionics Communications Inc. Leesburg, 2000, VA 20177, USA, ISBN 1-885544-10-3. 3. Moir, I. and Sea Bridge, A., AircraftSystems: Mechanical, Electrical and Avionics Sub Integration, AIAA Education Series, AIAA, 2001, ISBN 1-56347506-5. 4. arris, D., Ground Studies for Pilots: Flight Instruments and Automatic Flight Control Systems, sixth edition, Blackwell Science, 2004, ISBN 0-632-05951-6. 5. Avionics Systems Operation & Maintenance, 1994, Wasson, J. W., Jeppesen Sanderson Training Products, ISBN 0-89100-436-X. 6. Pallet, E..J., Aircraft Instruments & Integrated Systems, 1996, Longman scientific and technical.

X. COURSE PLAN: The course plan is meant as a guideline. There may probably be changes. Lecture No Course Learning Outcomes Topics to be covered Reference 1-2 3-4 Describing the important role of avionics in modern aircraft? Explanation of Core avionics UNIT-I: AVIONICS INTRODUCTION- AVIONICS STANDARDS Importance and role of avionics in modern aircraft core avionics and interface with pilot-aircraft state sensor, outside world sensor -task automation T1:1.1 T1:1.2 5-6 Explanation of ARNC and MIL specifications Requirements of avionics equipment and environmental, weight, reliability T1: 9.2.1.1 7-8 Introduction avionics equipment. Standardization and specifications of avionics equipment and -the ARNC and MIL specifications T1: 9.2.2 9-11 Describe Electrical and optical data bus Electrical and optical data bus -integrated modular avionics architectures-avionics packaging T1:9.2.3 12-14 Introduction about cockpit display units UNIT-II: DISPLAYS-MAN MACINE INTERACTION AND COMMUNICATION SYSTEMS T1: 2.1 15-17 Describing the different types of aircraft displays. Introduction to aircraft displays head up displays (UD)- basic principles T1:2.2 18-20 21-22 23 24-26 Explanation of head tracking Describing intelligent display management Explanation of voice and data communication -F, VF, UF Discuss audio management in flight elmet mounted displays, head tracking. ead down displays-civil cockpit, military cockpit. Solid state standby display. Data fusion in displays-intelligent display management Introduction to voice and data communication -F, VF, UF and SatelliteCommunication Data recorders Audio management in-flight entertainment T1:2.3-2.7 T1:2.8,2.9 T2:6.1 T2:6.2 27-28 Explanation of ACARS ACARS data communication. 29-30 31-33 34-36 37-39 Explanation of inertial sensors Explanation of Basic principles of gyroscopes and accelerometers Describing the optical gyroscopes-ring laser gyrosprinciples Explain Stable platform and strap down 40 Explain the GPS and GNSS UNIT-III: INERTIAL SENSORS AND GLOBAL POSITIONING SYSTEMS Basic principles of gyroscopes and accelerometers-angular momentum gyros-dynamically tuned gyro-micro machined vibrating mass rate gyro. Introduction to optical gyroscopes-ring laser gyros-principles. Specific force measurements with accelerometers, torque balance pendulous accelerometers Stable platform -strap down -errors in inertial and compensations. Global Navigational satellite -the global positioning system (GPS). T2:6.3 T1:5.1 T1:5.2 T1:5.2 T1:5.3 T1:6.5

41-43 Explain augmented satellite navigation description and basic principles-integration of GPS and INSdifferential GPS augmented satellite navigation T1:6.5 44-45 Describing navigation ranging UNIT-IV: NAVIGATION RANGING AND LANDING SYSTEMS T1:6.1 46-47 Explain Basic principles of navigation Introduction and Basic principles of navigation-types of navigation - Radio-navigation T1:6.1.2 48-50 Explain automatic direction finders. VF Omnirange, distance measuring equipment, automatic direction finders. T1:6.2 51-53 54 55-56 Analyze Inertial Navigation (INS) Discuss initial alignment and gyro-compassing Explain instrument landing 57-59 Discuss autoflight 60-61 Discuss Traffic alert and collision avoidance Attitude and heading reference. Inertial Navigation (INS) platform axes-angular rate corrections, acceleration correction, initial alignment and gyro compassing-strap down INS computing Aided INS-Kalman filters. Landing -localizer and glide-slope marker. Categories of instrument landing UNIT-V: SURVEILLANCE SYSTEMS AND AUTOFLIGT SYSTEMS Traffic alert and collision avoidance (TCAS)- Enhanced ground proximity warning T1:6.2 T1:6.2.3 T1:6.3 T1:7.1 T1:7.2 62-63 Explain Air traffic control Air traffic control -Mode S transponders-predictive wind shear warning -weather radar T1:7.3 65-66 Discuss auto-stabilization Longitudinal and lateral control and response of aircraftpowered flight controls-auto-stabilization T1:7.4 67-68 Discuss automatic landing Autopilots-principles-height control-heading control-ils coupled autopilot control-automatic landing T1:8.2 69-70 Explain autothrottle control Satellite landing guidance -speed control and autothrottle control. T1:8.2.6 71-73 Discuss Flight management Flight management -principles-flight planningnavigation and guidance T1:8.3 74-76 Discuss flight path optimization Flight path optimization and performance prediction-cost index. T1:8.3.4 XI. MAPPING COURSE OBJECTIVES LEADING TO TE ACIEVEMENT OF PROGRAM OUTCOMES AND PROGRAM SPECIFIC OUTCOMES Course Objectives Program Outcomes Program Specific Outcomes PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2 PSO3 PSO4 I S S II S S S S

III S S S IV S S S V S S S Supportive ighly related XII. MAPPING COURSE OUTCOMES LEADING TO TE ACIEVEMENT OF PROGRAM OUTCOMES AND PROGRAM SPECIFIC OUTCOMES Course Outcomes Program Outcomes Program Specific Outcomes PO1 PO2 PO3 PO4 PO5 PO6 PO7 PO8 PO9 PO10 PO11 PO12 PSO1 PSO2 PSO3 PSO4 1 S 2 S S S 3 S 4 S S 5 S 6 S S S 7 S 8 S 9 S S 10 S Supportive Prepared by: Mr. P.Anudeep, Assistant Professor Ms. M. Mary Thraza, Assistant Professor Mr. Naresh Eppakayala, Assistant Professor ighly related OD, Aeronautical Engineering