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Attitude and Heading Reference System with Sensor Fusion from Multiple Sensors using Adaptive Kalman Filter

Innovator Details

Innovator
Prof .Yatindra Nath Singh
Co-Developer / Co-Innovator
Dr.Naren Nayak

About

The project focuses on determining aircraft parameters relative to the runway, including attitude, direction, wind velocity vector, and position vector, for precise navigation and control.
Funding Organization
Funding Organization
Department of Science and Technology (DST)
Quick Information
TRL: Technology Readiness Level
4
TIH Name
TiHAN Foundation, IIT Hyderabad
Status
completed
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