Design and mathematical modeling of an amphibious quadcopter for versatile operations

Author:

Hosur Santosh1ORCID,Chikkanna N.2,Buradi Abdulrajak3,Barik Debabrata4ORCID,Paramasivam Prabhu56ORCID,Medhi Bhaskar Jyoti7,Bora Bhaskor Jyoti7ORCID

Affiliation:

1. Department of PG studies, Visvesvaraya Technological University, PG Centre Muddenhalli 1 , Chickballapur 562101, Karnataka, India

2. Department of Aerospace Propulsion Technology, Visvesvaraya Technological University, PG Centre Muddenhalli 2 , Chickballapur 562101, Karnataka, India

3. Department of Mechanical Engineering, Nitte Meenakshi Institute of Technology 3 , Bengaluru 560064, Karnataka, India

4. Department of Mechanical Engineering, Karpagam Academy of Higher Education 4 , Coimbatore 641021, India

5. Department of Research and Innovation, Saveetha School of Engineering, SIMATS 5 , Chennai, Tamilnadu 602105, India

6. Department of Mechanical Engineering, College of Engineering and Technology, Mattu University 6 , Mettu 318, Ethiopia

7. Assam Energy Institute, Sivasagar, A Centre of Rajiv Gandhi Institute of Petroleum Technology 7 , Sivasagar, Assam 785697, India

Abstract

Amphibious drone is an Unmanned Aerial Vehicle (UAV) capable of performing in both air and under water for application in various fields, such as marine, military, and underwater habitat research, but complexity in the design and provable mathematical model to withstand the arguably swift changes in the forces during the transition phase makes it difficult to build a sustainable UAV that can operate seamlessly in both media. Beginning with the mathematical principles and physical laws, the basic concept of operation is arrived at in the present study for both media (air and water) keeping the prime objective as developing a reliable drone design and mathematical model that will satisfactorily describe the behavior of the amphibious drone with accuracy by defining the coordinate system to describe the amphibious drone’s kinematics. Basic forces and torques are considered to explicitly describe the drone dynamics using Newton–Euler equations, and the final equation derived is the matrix Newton’s second law. Based on the mathematical model, the final design of the drone is arrived at considering the feasibility of withstanding forces, placement of commercial-off-the-shelf components, and the amount of thrust required to carry the seamless operation. A prototype is built with active buoyancy control technique to control the underwater depth of the drone, which clearly satisfies the design and mathematical model developed in this study.

Publisher

AIP Publishing

Reference35 articles.

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