New Delhi, Updated on Aug 25, 2021 15:49 IST
The Indian Institute of Technology (IIT) Kanpur is conducting a free online course on unmanned aerial vehicles (UAV) through the National Programme on Technology Enhanced Learning (NPTEL) platform.

ย The course isย best suited for UG and PG students who have a basic knowledge of aerodynamics. Those who wish to obtain certificates will have to pay Rs 1,000 and take an examination on October 24, 2021.ย 

IITK

The Indian Institute of Technology (IIT) Kanpur is conducting a free online course on unmanned aerial vehicles (UAV) through the Nationalย Programmeย on Technology Enhanced Learning (NPTEL) platform.ย Theย online course called design of fixed-wing UAV is an eight-week course and is free of cost. Theย programmeย began on August 23, 2021, and will go on till October 15, 2021. The course isย most suitedย for undergraduate and postgraduate students who have a basic knowledge of aerodynamics.ย Those who wish to obtain certificates will have to pay Rs 1,000 and take an examination on October 24, 2021.ย Candidates will only get e-certificates as no hard copies will be issued.ย 

The course will be conducted by Dr Subrahmanyamย Saderlaย who has a BTech in aeronautical engineering fromย Jawaharlal Nehru Technological Universityย (JNTU), Hyderabad in 2008, MTech and PhD in aerospace engineering from IIT Kanpur during 2010 and 2015, respectively.ย ย 

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What all will be taught during the course

  • Introduction to fixed-wing UAVs, design, and basic design parameters.ย 
  • Designย  Algorithm: Case study, and design algorithm: mission requirements.ย 
  • Feasibleย  design parameters, and configuration layout: Airfoil selection,ย  configuration layout: Planform geometry selection.ย 
  • Weightย  and CG estimation, analytical parameter estimation, and analyticalย  parameter estimation.ย 
  • Performanceย  and stability analysis, simulation and detailedย sising.ย 
  • Estimationย  of inertial properties using 3D modelling, and prototypeย  fabrication.ย 
  • Windย  tunnel testing, and aerodynamicย characterisationย  through wind tunnel testing.ย 

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