18AS733: Air and Missile Defence Systems AS Syllabus for BE 7th Sem 2018 Scheme VTU (Professional Elective-2)

Air and Missile Defence Systems detailed Syllabus for Aerospace Engineering (AS), 2018 scheme has been taken from the VTUs official website and presented for the VTU students. For Course Code, Subject Names, Teaching Department, Paper Setting Board, Theory Lectures, Tutorial, Practical/Drawing, Duration in Hours, CIE Marks, Total Marks, Credits and other information, visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.

For all the other VTU AS 7th Sem Syllabus for BE 2018 Scheme, visit Aerospace Engineering 7th Sem 2018 Scheme.

For all the (Professional Elective-2) subjects refer to Professional Elective-2 Scheme. The detail syllabus for air and missile defence systems is as follows.

Course Objectives:

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Module 1

Missile Systems Introduction History of guided missile for defence applications- Classification of missiles- The Generalized Missile Equations of Motion- Coordinate Systems- Lagrange’s Equations for Rotating Coordinate Systems- Rigid-Body Equations of Motion-missile system elements, missile ground systems.

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 agilityPitch Autopilot Design, Pitch-Yaw-Roll Autopilot Design.

Module 3

Module 4

Strategic Missiles Introduction, The Two-Body Problem, Lambert’s Theorem, First-Order Motion of a Ballistic Missile , Correlated Velocity and Velocity-to-Be-Gained Concepts, Derivation of the Force Equation for Ballistic Missiles, Atmospheric Reentry, Ballistic Missile Intercept, Threat analysis for Boost phase interception -Typical assessment errors. Missile Tracking Equations of Motion, Introduction to Cruise Missiles , The Terrain-Contour Matching (TERCOM) Concept.

Module 5

Interception Guidance And Interception Of Maneuvering Targets: Proportional navigation geometry -proportional navigation linearized system and zero miss distance proportional navigation-optimal guidance law-mathematical modeling of pursuit-evasion-solution with constrained evader-stochastic analysis 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:

Question paper pattern:

The question paper will have ten full questions carrying equal marks.
Each full question will be for 20 marks.
There will be two full questions (with a maximum of four sub- questions) from each module.
Each full question will have sub- question covering all the topics under a module.
The students will have to answer five full questions, selecting one full question from each module.

Text Books:

Missile Guidance and control systems Siouris, G.M Springer 2003
Automatic Control of Aircraft and Missiles Blakelock, J. H John Wiley & Sons 2nd Edition,1990

Reference Books:

For the detail Syllabus of all other subjects of BE (AS) 7th Sem, visit Aerospace Engineering 7th Sem Subjects.

For all (CBSE & Non-CBSC) BE/B.Tech results, visit VTU BE/B.Tech all semester results.

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