Missile Design AS 8th Sem Syllabus for VTU BE 2017 Scheme

Missile Design detail syllabus for Aerospace Engineering (As), 2017 scheme is taken from VTU official website and presented for VTU students. The course code (17AS82), and for exam duration, Teaching Hr/week, Practical Hr/week, Total Marks, internal marks, theory marks, duration and credits do visit complete sem subjects post given below.

For all other as 8th sem syllabus for be 2017 scheme vtu you can visit AS 8th Sem syllabus for BE 2017 Scheme VTU Subjects. The detail syllabus for missile design is as follows.

Course Objectives:

This course will enable students to

1. Understand the basic of missile systems.
2. Comprehend the Missile airframe, autopilots and control.
3. Acquire the knowledge on missile guidance and delivery systems.

Module 1

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Module 2

Missile Airframes, Autopilots and Control: Missile aerodynamics, Force Equations, Moment Equations, Phases of missile flight. Missile control configurations. Missile Mathematical Model. Autopilots, Definitions, Types of Autopilots, Example Applications. Open-loop autopilots. Inertial instruments and feedback. Autopilot response, stability, and agility, Pitch Autopilot Design, Pitch-Yaw-Roll Autopilot Design.

Module 3

Missile Guidance Laws: Tactical Guidance Intercept Techniques, Derivation of the fundamental Guidance Equations, explicit, Proportional Navigation, Augmented Proportional Navigation, beam riding, bank to turn missile guidance, Three-Dimensional Proportional Navigation, comparison of guidance system performance, Application of Optimal Control of Linear Feedback Systems.

Module 4

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Module 5

Weapon Delivery Systems: Weapon Delivery Requirements, Factors Influencing Weapon Delivery Accuracy, Unguided Weapons, The Bombing Problem, Guided Weapons, Integrated Flight Control in Weapon Delivery, Missile Launch Envelope, Mathematical Considerations Pertaining to the Accuracy of Weapon Delivery Computations.

Course Outcomes:

After studying this course, students will be able to:

1. Classify the missile systems.
2. Configure the missile control using the design and control laws.
3. Identify the weapon delivery systems.

Graduate Attributes (as per NBA):

• Engineering Knowledge. Problem Analysis. Design / development of solutions Interpretation of data

Question paper pattern:

• The question paper will have ten questions.
• Each full question consists of 16 marks.
• There will be 2 full questions (with a maximum of four sub questions) from each module.
• Each full question will have sub questions covering all the topics under a module.
• The students will have to answer 5 full questions, selecting one full question from each module.

Text Books:

1. Siouris, G.M. “Missile Guidance and control systems”, Springer, Reprinted edition, 2010, ISBN-13: 978-1441918352
2. Blakelock, J. H.; Automatic Control of Aircraft and Missiles,John Wiley & Sons, 2nd Edition,1990

Reference Books:

1. Fleeman, Eugene L, Tactical Missile Design, AIAA Education series, First Edition, 2001,ISBN-13: 978-1563474941
2. Garnell, P., “Guided Weapon Control Systems”, 2nd Edition, Pergamon Press, 1980.
3. Joseph Ben Asher and Isaac Yaesh Advances in Missile Guidance Theory AIAA Education series, 1998,ISBN-13: 978-1563472756
4. Paul Zarchan Tactical and Strategic Missile Guidance AIAA Education series,6th revised edition,2012,ISBN-13: 978-1600868948

For detail syllabus of all other subjects of BE As, 2017 scheme do visit As 8th Sem syllabus for 2017 scheme.

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