Coordinate systems, Attitude dynamics and control, Rotational kinematics, Direction cosine matrix, Euler angles, Euler’s eigen axis rotation, Quaternions, Rigid body dynamics of launch vehicle, Angular momentum, Inertia matrix, Principal axes, Derivation of dynamic equations, Effect of aerodynamics,  structural dynamics and flexibility, propellant sloshing, actuator dynamics, gimballed engine dynamics, External forces and moments, Linear model for Aero‐structure‐control‐slosh interaction studies.

Same as Reference

1. J.H.Blakelock, Automatic control of Aircraft and Missiles, Wiley India,1991
2. A.L.Greensite, Control Theory Vol. II- Analysis and Design of Space Vehicle Flight Control Systems, Spartan Books, 1970
3. N V Kadam ,Practical design of flight control systems for launch vehicles and Missiles , Allied Publishers Pvt. Ltd., 2009
4. Brian L. Stevens, Frank L. Lewis, Aircraft Control and Simulation, Wiley, 2003
5. K. J. Ball, G. F. Osborne, Space vehicle dynamics, Clarendon P., 1967
6. A. L. Greensite, Analysis and Design of Space Vehicle Flight Control Systems – Short Period Dynamics, Vol 1, NASA
7. A. L. Greensite, Analysis and Design of Space Vehicle Flight Control Systems, -- Trajectory Equations Vol 2, 1967, NASA