Proceedings of the Conference on Advances in Communication and Control Systems (CAC2S 2013)

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Avionics System Design of Vertical Take off and Landing UAV

Authors
Amit Joshi, Sakshi Kukreti
Corresponding Author
Amit Joshi
Available Online April 2013.
Abstract

This paper presents the details of avionics system design of a quadrotor. It uses the direction cosine matrix approach to identify the coordinates of the quadrotor and then using PID controller it tries to minimize the drifting error. The aim of the paper is to develop a system which uses a small amount a processing power and still remains stable. This reduces the cost of the system and allows the users to develop the system further more. PID controller has been implemented in the algorithm as it is the simplest controller widely used in rotor industry.

Copyright
© 2013, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the Conference on Advances in Communication and Control Systems (CAC2S 2013)
Series
Advances in Intelligent Systems Research
Publication Date
April 2013
ISBN
null
ISSN
1951-6851
Copyright
© 2013, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

risenwbib
TY  - CONF
AU  - Amit Joshi
AU  - Sakshi Kukreti
PY  - 2013/04
DA  - 2013/04
TI  - Avionics System Design of Vertical Take off and Landing UAV
BT  - Proceedings of the Conference on Advances in Communication and Control Systems (CAC2S 2013)
PB  - Atlantis Press
SP  - 35
EP  - 41
SN  - 1951-6851
UR  - https://www.atlantis-press.com/article/6274
ID  - Joshi2013/04
ER  -