Adaptive PID Control via Sliding Mode for Position Tracking of Quadrotor MAV: Simulation and Real-Time Experiment Evaluation

Author:

Noordin Aminurrashid12ORCID,Mohd Basri Mohd Ariffanan1,Mohamed Zaharuddin1

Affiliation:

1. Faculty of Electrical Engineering, Universiti Teknologi Malaysia, UTM, Johor Bahru 81310, Johor, Malaysia

2. Faculty of Electrical and Electronic Engineering Technology, Universiti Teknikal Malaysia Melaka, Hang Tuah Jaya, Durian Tunggal, Melaka 76100, Malacca, Malaysia

Abstract

The lightweight nature of micro air vehicles (MAVs) makes them highly sensitive to perturbations, thus emphasizing the need for effective control strategies that can sustain attitude stability throughout translational movement. This study evaluates the performance of two controllers (Proportional-Integral-Derivative (PID) and Adaptive PID based on Sliding Mode Control (SMC)) on a MAV that is subjected to external disturbances. These controllers are initially simulated using MATLAB®/Simulink™ and then implemented in real-time on the Parrot Mambo Minidrone. The observation on the waypoint follower and the orbit follower in both simulation and experiment showed that the Adaptive PID (APID) controller is more effective and robust than the PID controller against external disturbances such as wind gusts. The study provides evidence of the potential of the APID control scheme in enhancing the resilience and stability of MAVs, making them suitable for various applications including surveillance, search and rescue, and environmental monitoring.

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference30 articles.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A Sensor Fusion Approach to Observe Quadrotor Velocity;Sensors;2024-06-03

2. Attitude and Altitude Control of Quadrotor MAV using FOPID Controller;Communications in Computer and Information Science;2023-10-13

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