Development and Automation of Fixed Wing UAV for Reconnaissance Mission with FPV Capability-Reference-Cited by-同舟云学术

Development and Automation of Fixed Wing UAV for Reconnaissance Mission with FPV Capability

Published:2022-12-02 Issue:4 Volume:14 Page:111-118
ISSN:2247-4528
Container-title:INCAS BULLETIN
language:en
Short-container-title:INCAS BULLETIN

Author:

PREM ANAND T. P.¹,ABISHEK K.²,KRISHNA KAILASH R.³,NITHIYANANTHAM K. K.⁴

Affiliation:

1. Department of Aeronautical Engineering, Rajalakshmi Engineering College, Thandalam, Chennai 602 105, India, premanand.tp@rajalakshmi.edu.in

2. Department of Aeronautical Engineering, Rajalakshmi Engineering College, Thandalam, Chennai 602 105, India, abishek.k.2018.aero@rajalakshmi.edu.in

3. Department of Aeronautical Engineering, Rajalakshmi Engineering College, Thandalam, Chennai 602 105, India, krishnakailash.r.2018.aero@rajalakshmi.edu.in

4. Department of Aeronautical Engineering, Rajalakshmi Engineering College, Thandalam, Chennai 602 105, India, nithiyanantham.kk@rajalakshmi.edu.in

Abstract

Today's military missions require pre-emptive knowledge of hostile activities in and around the conflict zone. Using a multi rotor UAV for Reconnaissance has many disadvantages, such as cost, range, reduced maneuverability and much more. The main objective is to make the UAV completely autonomous, with the transmitter on standby. By entering the flight plan into the Ground Control System, the UAV will complete the assigned mission autonomously and will be guided by an operational flight plan wherein active waypoints are plotted in the GCS. The GCS can be linked to the Telemetry and the Global Positioning System to have a complete knowledge of the UAV location.

Publisher

INCAS - National Institute for Aerospace Research Elie Carafoli

Subject

Aerospace Engineering,Control and Systems Engineering

Reference9 articles.

1. [1] S. S. Hegde, R. Kishan, S. Nayak and N. Chavan, A Systematic Approach for Designing, Analyzing and Building a Model RC Plane, International Journal of Engineering Research & Technology, vol. 3, no. 12, 2014.

2. [2] W. Lee, J. Y. Lee, J. Lee, K. Kim, S. Yoo, S. Park and H. Kim, Ground control system based routing for reliable and efficient multi-drone control system, Applied Sciences (Switzerland), vol. 8, no. 11, 2018.

3. [3] Y. Zhao, H. Miu, J. Ma, and H. Du, Design of the Reconnaissance UAV based on TGAM, Journal of Physics, vol. 1771, no. 1, 2021.

4. [4] I. Y. Hussain and M. S. Abood, 2016. Experimental study of CLARK-Y smoothed inverted wing with ground effect, International Journal of Computer Applications, vol. 147, no. 1, 2016.

5. [5] K. D. Patel, C. S. Jayaraman, and S. K. Maurya, Selection of BLDC Motor and Propeller for Autonomous Amphibious Unmanned Aerial Vehicle, WSEAS Transactions on Systems and Control, 10, 179-185, 2015.