{"id":58854,"date":"2023-09-05T13:15:54","date_gmt":"2023-09-05T13:15:54","guid":{"rendered":"https:\/\/www.inspirenignite.com\/anna-university\/as3016-missile-guidance-and-control-syllabus-for-aerospace-engg-2021-regulation-professional-elective-vii\/"},"modified":"2023-09-05T13:15:54","modified_gmt":"2023-09-05T13:15:54","slug":"as3016-missile-guidance-and-control-syllabus-for-aerospace-engg-2021-regulation-professional-elective-vii","status":"publish","type":"post","link":"https:\/\/www.inspirenignite.com\/anna-university\/as3016-missile-guidance-and-control-syllabus-for-aerospace-engg-2021-regulation-professional-elective-vii\/","title":{"rendered":"AS3016: Missile Guidance and Control syllabus for Aerospace Engg 2021 regulation (Professional Elective-VII)"},"content":{"rendered":"

Missile Guidance and Control detailed syllabus for Aerospace Engineering (Aerospace Engg) for 2021 regulation curriculum has been taken from the Anna Universities<\/a> official website and presented for the Aerospace Engg students. For course code, course name, number of credits for a course and other scheme related information, do visit full semester subjects post given below. <\/p>\n

For Aerospace Engineering 6th Sem scheme and its subjects, do visit Aerospace Engg 6th Sem 2021 regulation scheme<\/a>. For Professional Elective-VII scheme and its subjects refer to Aerospace Engg Professional Elective-VII syllabus scheme<\/a>. The detailed syllabus of missile guidance and control is as follows. <\/p>\n

Course Objectives:<\/h4>\n

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Unit I<\/h4>\n

INTRODUCTION TO MISSILE SYSTEMS
\nHistory of guided missile for defence applications- Classification of missiles- Generalized Missile Equations of Motion- Coordinate Systems- Lagrange\u2019s Equations for Rotating Coordinate Systems-Rigid-Body Equations of Motion-missile system elements, missile ground systems.\n<\/p>\n

Unit II<\/h4>\n

MISSILE AIRFRAMES, AUTOPILOTS AND CONTROL
\nMissile aerodynamics- Force Equations, Moment Equations, Phases of missile flight. Missile control configurations. Missile Mathematical Model. Autopilots \u2014 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.\n<\/p>\n

Unit III<\/h4>\n

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Unit IV<\/h4>\n

STRATEGIC MISSILES
\nIntroduction, Two-Body Problem, Lambert\u2019s 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 Re-entry, Ballistic Missile Intercept, Missile Tracking Equations of Motion, Introduction to Cruise Missiles, Terrain-Contour Matching (TERCOM) Concept.\n<\/p>\n

Unit V<\/h4>\n

WEAPON DELIVERY SYSTEMS
\nWeapon Delivery Requirements, Factors Influencing Weapon Delivery Accuracy, Unguided Weapons, Bombing Problem, Guided Weapons, Integrated Flight Control in Weapon Delivery, Missile Launch Envelope, Mathematical Considerations Pertaining to the Accuracy of Weapon Delivery Computations.\n<\/p>\n

Course Outcomes:<\/h4>\n

On successful completion of this course, the student will be able to<\/p>\n