Anna University Syllabus - Anna University ME Syllabus
AS7201 MISSILE GUIDANCE AND CONTROL Syllabus | Anna University ME Aerospace Technology (LVT) Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aerospace Technology(Launch Vehicle Technology), Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics.
It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AS7201 MISSILE GUIDANCE AND CONTROL L T P C 3 0 0 3
OUTCOME:
Upon completion of this course, students will understand the advanced concepts of missile guidance
and control to the engineers and to provide the necessary mathematical knowledge that are needed in
understanding the physical processes. The students will have an exposure on various topics such as
missile systems, missile airframes, autopilots, guidance laws and will be able to deploy these skills
effectively in the understanding of missile guidance and control.
UNIT I MISSILE SYSTEMS INTRODUCTION 8
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.
UNIT II MISSILE AIRFRAMES, AUTOPILOTS AND CONTROL 9
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.
UNIT III MISSILE GUIDANCE LAWS 10
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.
UNIT IV STRATEGIC MISSILES 10
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, Missile Tracking Equations of Motion,
Introduction to Cruise Missiles , The Terrain-Contour Matching (TERCOM) Concept.
UNIT V WEAPON DELIVERY SYSTEMS 8
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.
L : 45, TOTAL: 45 PERIODS
REFERENCES:
1. Siouris, G.M. "Missile Guidance and control systems", Springer, 2003.
2. Blakelock, J. H.; Automatic Control of Aircraft and Missiles, 2nd Edition, John Wiley & Sons, 1990.
3. Fleeman, Eugene L.; Tactical Missile Design, First Edition, AIAA Education series, 2001.
4. Garnell, P., "Guided Weapon Control Systems", 2nd Edition, Pergamon Press, 1980.
5. Joseph Ben Asher and Isaac Yaesh “Advances in Missile Guidance Theory” AIAA Education
series, 1998
6. Paul Zarchan “Tactical and Strategic Missile Guidance” AIAA Education series,2007
AS7201 MISSILE GUIDANCE AND CONTROL L T P C 3 0 0 3
OUTCOME:
Upon completion of this course, students will understand the advanced concepts of missile guidance
and control to the engineers and to provide the necessary mathematical knowledge that are needed in
understanding the physical processes. The students will have an exposure on various topics such as
missile systems, missile airframes, autopilots, guidance laws and will be able to deploy these skills
effectively in the understanding of missile guidance and control.
UNIT I MISSILE SYSTEMS INTRODUCTION 8
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.
UNIT II MISSILE AIRFRAMES, AUTOPILOTS AND CONTROL 9
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.
UNIT III MISSILE GUIDANCE LAWS 10
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.
UNIT IV STRATEGIC MISSILES 10
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, Missile Tracking Equations of Motion,
Introduction to Cruise Missiles , The Terrain-Contour Matching (TERCOM) Concept.
UNIT V WEAPON DELIVERY SYSTEMS 8
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.
L : 45, TOTAL: 45 PERIODS
REFERENCES:
1. Siouris, G.M. "Missile Guidance and control systems", Springer, 2003.
2. Blakelock, J. H.; Automatic Control of Aircraft and Missiles, 2nd Edition, John Wiley & Sons, 1990.
3. Fleeman, Eugene L.; Tactical Missile Design, First Edition, AIAA Education series, 2001.
4. Garnell, P., "Guided Weapon Control Systems", 2nd Edition, Pergamon Press, 1980.
5. Joseph Ben Asher and Isaac Yaesh “Advances in Missile Guidance Theory” AIAA Education
series, 1998
6. Paul Zarchan “Tactical and Strategic Missile Guidance” AIAA Education series,2007
No comments:
Post a Comment
Any doubt ??? Just throw it Here...