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UAV Design - Part II
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Overview
This course introduces the designing and sizing process (Simulation/Experimental) for fixed – wing UAV technology, integrated with its performance and stability analysis (Static & Dynamic) and prototype testing
free
Type: Online
This course includes
- 8 weeks long
- Paid Certificate Available
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free
Type: Online
This course includes
- 8 weeks long
- Paid Certificate Available
Taken this course?
Share your experience with other students
UAV Design - Part II
Created by -
0.00
(0 ratings)
Start Date: August 16th 2020
Course Description
This course introduces the designing and sizing process (Simulation/Experimental) for fixed – wing UAV technology, integrated with its performance and stability analysis (Static & Dynamic) and prototype testing
INTENDED AUDIENCE :Undergraduate and postgraduate students
PREREQUISITES :Introduction to Aerodynamics/Flight Mechanics
INDUSTRIES SUPPORT :DRDO, HAL, Boeing, Airbus, Bell, McDonnell Douglas, UAV Factory, Lockheed Martin
Course Structure
COURSE LAYOUT
Week 1: Review of the concepts covered in first part of the courseWeek 2: Understanding the static stability of various UAVs. Significance of location of Neutral point and Centre of gravity for a stable flight.Week 3: Approach for wing design and airfoil selection with examplesWeek 4: Tail sizing, control surface sizing and significance of tail volume ratio with examples
Week 5: Developing subroutine for design processWeek 6: Design example for conventional takeoff fixed wing UAV for various mission requirementsWeek 7: Design example for hand launch fixed wing UAV for various mission requirementWeek 8: Design example for VTOL fixed wing UAV for various mission requirement
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About the Instructor
Prof. Saderla Subrahmanyam,Indian Institute of Technology Kanpur
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