NMPC-PID based new control structure design for altitude and attitude stabilization of non-linear quad-rotor type unmanned aerial vehicles (UAV)

Quad-rotor typed unmanned aerial vehicles (UAV) are rotorcraft that has four propellers. In this design there are two arms and each arm has two propellers at their end.. It has complex controlling structure, that is why this rotorcraft is overall non-linear in nature. Hence, it creates a lot of dif...

Full description

Saved in:
Bibliographic Details
Main Author: Muhammad Hassan, Tanveer
Format: Thesis
Language:English
Subjects:
Online Access:http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/44117/1/p.1-24.pdf
http://dspace.unimap.edu.my:80/xmlui/bitstream/123456789/44117/2/full%20text.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items