四轴飞行器
控制理论(社会学)
非线性系统
模型预测控制
计算机科学
观察员(物理)
控制工程
动力学(音乐)
自适应控制
车辆动力学
动量(技术分析)
控制(管理)
工程类
物理
人工智能
财务
航空航天工程
经济
汽车工程
量子力学
声学
作者
Bryan S. Guevara,Luis F. Recalde,Viviana Moya,José Varela-Aldás,Daniel Gandolfo,Juan Marcos Toibero
出处
期刊:IEEE Access
[Institute of Electrical and Electronics Engineers]
日期:2024-01-01
卷期号:12: 77121-77132
标识
DOI:10.1109/access.2024.3407684
摘要
This article proposes an enhancement to estimate unmodeled dynamics within the simplified dynamic model of a quadcopter by integrating three key methodologies: Nonlinear Model Predictive Control (NMPC), a Momentum Observer Dynamics (MOD), and an adaptive control law. Termed as Adaptive NMPC with MOD, this integrated approach leverages NMPC, implemented using the CasADi framework, for real-time decision-making, while the momentum observer facilitates system state estimation and uncertainty mitigation. Simultaneously, the adaptive control law adjusts parameters to estimate errors in unmodeled dynamics. Through digital twin and Model in Loop (MiL) simulations, the effectiveness of this framework is demonstrated. Specifically, the study focuses on the simplified quadcopter model, acknowledging often overlooked inherent dynamics resulting from the simplification by not considering the nonlinearities induced by the drone's attitude angles. Addressing these unmodeled dynamics is critical, and the Adaptive NMPC with MOD method emerges as a robust solution, showcasing its potential across various scenarios.
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