Title :
Design of effective landing mechanism for fully autonomous Unmanned Aerial Vehicle
Author :
Nagarjuna, Kotha ; Suresh, G.R.
Author_Institution :
M.E Embedded Syst. Technol., Easwari Eng. Coll., Chennai, India
Abstract :
Aerial Vehicles have always been an area of extensive research in terms of stabilization and attaining autonomous status for itself. Aerial Vehicles are of various types like quadcopter, helicopter, multi-rotors, drones, etc. Each of the Aerial Vehicle has its own principle of operation and working environment. Quadcopter is the most preferred of the aerial vehicles owing to its simplicity and ease of control. Realizing a quadcopter is much easier and requires less cost. Unmanned Aerial Vehicles requires the aerial vehicle to take decision on its own without any user intervention. This includes the ability of the quadcopter to take off and land safely. The main challenge in the autonomous feature of the quadcopter is to land the UAV in the destination without an operator manually controlling the operation. In this project the landing mechanism of the UAV is monitored using gyroscope and accelerometer without any physical aid and image processing. The altitude value is monitored and the speed of the motors is decreased accordingly. The drones are completely autonomous and could also be instructed to follow a predefined path along the LoC from a remote computer. A predefined map of the surveillance area is fed as co-ordinates into the ARM Cortex series controlled boards. So moving from one co-ordinate location to another will be in a predefined path. A fail safe mechanism is also incorporated so that the working motors make up for the lost motor by running at 120% of the rated speed of the motor.
Keywords :
accelerometers; autonomous aerial vehicles; entry, descent and landing (spacecraft); gyroscopes; helicopters; microprocessor chips; space vehicles; ARM Cortex series controlled board; LoC; accelerometer; drone; effective landing mechanism; fully autonomous unmanned aerial vehicle; gyroscope; helicopter; image processing; multirotor; quadcopter; remote computer; Monitoring; Pulse width modulation; Unmanned aerial vehicle; fail-safe; landing mechanism; quadcopter; stabilization;
Conference_Titel :
Signal Processing, Communication and Networking (ICSCN), 2015 3rd International Conference on
Conference_Location :
Chennai
Print_ISBN :
978-1-4673-6822-3
DOI :
10.1109/ICSCN.2015.7219864