M.Tech (Structures and Design)
The M.Tech in Structures and Design at the Indian Institute of Space Science and Technology (IIST) is a postgraduate programme aimed at developing expertise in the analysis, design, and optimization of aerospace structures. This programme provides in-depth knowledge of advanced materials, structural mechanics, and design methodologies crucial to modern aerospace systems.
M.Tech (Aerodynamics and Flight Mechanics)
The M.Tech in Aerodynamics and Flight Mechanics at the Indian Institute of Space Science and Technology (IIST) is a specialized postgraduate programme focused on the theoretical and practical aspects of fluid dynamics, aerodynamic design, and the dynamics and control of flight vehicles.
Even Semester Jan-June 2024-2025
Programme type
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Avionics
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Aerospace Engineering
Semester
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Chemistry
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Earth and Space Sciences
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Mathematics
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Physics
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Time Table for DD - Sem VIII
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Mathematical Methods in Aerospace Engineering
Review of Ordinary Differential Equations: analytical methods, stability – Fourier series, orthogonal functions, Fourier integrals, Fourier transform – Partial Differential Equations: first-order PDEs, method of characteristics, linear advection equation, Burgers’ equation, shock formation, Rankine-Hogoniot jump condition; classification, canonical forms; Laplace equation, min-max principle, cylindrical coordinates; heat equation, method of separation of variables, similarity transformation method; wave equation, d’Alembert solution – Calculus of Variations: standard variational problems, E
Flight Dynamics and Control
Equations of Motion: rigid body dynamics, coordinate transformation, Euler angle & quaternion formulation – Dynamics of Generic Fixed Wing Aircraft: 6-DoF equations of motion, linearized equations of motion, linearised longitudinal & lateral equations, aerodynamic derivatives – LTI sys- tem basics – Stability of Uncontrolled Motion: linearized longitudinal & lateral dynamics, modes of motion – Response to Control Inputs: transfer function, step response & frequency response charac- teristics – Feedback Control: stability augmentation, PID control, root-locus technique for co