Avionics System Design of Vertical Take off and Landing UAV

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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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  -