Classification of UAV

Module 2

UAVs can be classified according to the type of wing and aerodynamic configuration they use. The wing configuration significantly influences the UAV’s stability, endurance, maneuverability, payload capacity, and mission role.

UAV Classification Dashboard
UAV Classification Explorer
Click → Subtype → Explore UAV Function & Real Applications
Configuration
Weight
Altitude & Endurance
Mission

Fixed Wing

Single Rotor

Multirotor

Hybrid VTOL

Nano

Micro

Small

Medium

Large

VLA-SE

LASE

LALE

MALE

HALE

Very Close Range

Close Range

Short Range

Medium Range

Long Range

Select a subtype to view UAV details

Reference
1. S.S. Chin. Missile Configuration Design. McGraw Hill, 1961.

2. Mark Pinney Aerodynamics of Missiles and Rockets. McGraw-Hill Education, 2013.

3. Marvin Hobbs Fundamentals of Rockets, Missiles, and Spacecraft. J.F. Rider, 1962.

4. Sethunathan, P., Sugendran, R. N., & Anbarasan, T. Aerodynamic Configuration design of a missile at Int J Eng Res & Technol (IJERT), 2015.

5. Jack N. Nielsen Missile Aerodynamics. NIELSEN ENGINEERING & RESEARCH, INC, 1988.

6. Siouris, George Missile Guidance and Control Systems. Springer New York, 2006.
Classification of UAVs by Dr Aishwarya Dhara
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