Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework

In this paper, we deal with a Bicopter drone that has two thrusters and two tilting servos. Both the position and attitude dynamics of Bicopter are globally expressed on the Special Euclidean group SE3. A simple control allocation method is proposed to map between the control wrench and actuator inp...

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Main Authors: Vijay Reddy Vundela, Vijay Muralidharan
Format: Article
Language:English
Published: Wiley 2024-01-01
Series:Journal of Robotics
Online Access:http://dx.doi.org/10.1155/2024/5552493
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author Vijay Reddy Vundela
Vijay Muralidharan
author_facet Vijay Reddy Vundela
Vijay Muralidharan
author_sort Vijay Reddy Vundela
collection DOAJ
description In this paper, we deal with a Bicopter drone that has two thrusters and two tilting servos. Both the position and attitude dynamics of Bicopter are globally expressed on the Special Euclidean group SE3. A simple control allocation method is proposed to map between the control wrench and actuator inputs for the Bicopter. A geometric nonlinear attitude and altitude tracking controller is developed for the Bicopter and the asymptotic stability analysis is performed using the Lyapunov method for the closed-loop nonlinear system. The performance of the proposed altitude and attitude stabilization controller is validated through experimental hardware developed in-house. The attitude controller performance is validated through simulations and shown to be comparable against an linear matrix inequality-based control law.
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institution Kabale University
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language English
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spelling doaj-art-77bee1263ed244dca83f231dfb0842e42025-02-03T05:56:55ZengWileyJournal of Robotics1687-96192024-01-01202410.1155/2024/5552493Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric FrameworkVijay Reddy Vundela0Vijay Muralidharan1Electrical EngineeringElectrical EngineeringIn this paper, we deal with a Bicopter drone that has two thrusters and two tilting servos. Both the position and attitude dynamics of Bicopter are globally expressed on the Special Euclidean group SE3. A simple control allocation method is proposed to map between the control wrench and actuator inputs for the Bicopter. A geometric nonlinear attitude and altitude tracking controller is developed for the Bicopter and the asymptotic stability analysis is performed using the Lyapunov method for the closed-loop nonlinear system. The performance of the proposed altitude and attitude stabilization controller is validated through experimental hardware developed in-house. The attitude controller performance is validated through simulations and shown to be comparable against an linear matrix inequality-based control law.http://dx.doi.org/10.1155/2024/5552493
spellingShingle Vijay Reddy Vundela
Vijay Muralidharan
Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework
Journal of Robotics
title Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework
title_full Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework
title_fullStr Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework
title_full_unstemmed Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework
title_short Nonlinear Attitude and Altitude Trajectory Tracking Control of a Bicopter UAV in Geometric Framework
title_sort nonlinear attitude and altitude trajectory tracking control of a bicopter uav in geometric framework
url http://dx.doi.org/10.1155/2024/5552493
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AT vijaymuralidharan nonlinearattitudeandaltitudetrajectorytrackingcontrolofabicopteruavingeometricframework