Week 1: Introduction to Unmanned Aerial Vehicles, Types of UAVs, applications, design process and design goals
Week 2: UAS as a System of Systems, description of each sub-system and its role, fixed wing primary control, introduction to aerodynamics
Week 3: Aerodynamic performance – lift, drag, L/D, effect of pitching moment, wing loading for UAVs, stalling speed,
Week 4: Concept of load factor, range, endurance, rate of climb etc. for fixed wing UAVs with fuel as well as battery power
Week 5: Low Reynolds number aerodynamics, Propeller Theory
Week 6: Introduction to rotary wing aerodynamics, momentum theory in hover, definition of nomenclature for rotary wing systems
Week 7: Momentum theory in climb, descent and forward flight
Week 8: Blade element theory, rotors in axial and edgewise flight
Week 9: Blade Element Momentum Theory, Prandtl tip loss function.
Week 10: Performance of rotary wing UAVs, range, endurance, rate of climb, maximum speed
Week 11: Introduction to flapping wing UAVs and unsteady aerodynamics
Week 12: Flight dynamics of UAVs with focus on Quadrotor Flight dynamics
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