DocumentCode :
2169769
Title :
Design and Development of an Y4 Copter Control System
Author :
Hossain, Md Shafayat ; Kabir, Ariyan M. ; Mazumder, Pratyai ; Aziz, Ahmedullah ; Hassan, Masudul ; Islam, Md Azizul ; Saha, Pran Kanai
Author_Institution :
Dept. of Electr. & Electron. Eng., Bangladesh Univ. of Eng. & Technol., Dhaka, Bangladesh
fYear :
2012
fDate :
28-30 March 2012
Firstpage :
251
Lastpage :
256
Abstract :
The y4 copter is intended to be a UAV (Unmanned Aerial Vehicle) with autonomous subsystems. Automation is implemented in case of maintaining the desired roll, pitch and yaw. An improved algorithm that uses Quaternion is implemented to determine Euler angles avoiding Gimbal lock. It has a self-stabilization system achieved using Proportional Integral Derivative (PID) control system. A custom remote is built to communicate with the y4 copter using XBee modules which offer long range and security. Secured data transmission between the controller and the copter makes it suitable for military applications. Perhaps the most significant purpose of this y4 copter is to exercise a low cost and efficient engineering design with total automation considering all possible aerodynamics which is intended to be the first y4 copter built in the Indian subcontinent.
Keywords :
aerodynamics; aircraft control; autonomous aerial vehicles; computational geometry; design engineering; helicopters; military aircraft; mobile robots; self-adjusting systems; stability; three-term control; vehicle dynamics; Euler angles; Indian subcontinent; PID control system; UAV; XBee modules; Y4 copter control system; aerodynamics; autonomous subsystems; engineering design; gimbal lock avoidance; military applications; military surveillance; pitch maintenance; proportional integral derivative control system; quadrotor; roll maintenance; secured data transmission; self-stabilization system; unmanned aerial vehicle; yaw maintenance; Accelerometers; Control systems; Equations; Force; Mathematical model; Rotors; Sensors; IMU; PID; XBee; accelerometer; gyro; lift; pitch; quaternion; roll; thrust; yaw;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Modelling and Simulation (UKSim), 2012 UKSim 14th International Conference on
Conference_Location :
Cambridge
Print_ISBN :
978-1-4673-1366-7
Type :
conf
DOI :
10.1109/UKSim.2012.43
Filename :
6205457
Link To Document :
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