Avionics System Design of Vertical Take off and Landing UAV
Amit Joshi, Sakshi Kukreti
Available Online April 2013.
- 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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
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-2013 PB - Atlantis Press SP - 35 EP - 41 SN - 1951-6851 UR - https://www.atlantis-press.com/article/6274 ID - Joshi2013/04 ER -