Control Simulation of Flapping-Wing Micro Aerial Vehicle Based on Multi-level Optimization Model Predictive Control

In this paper, a control algorithm using multi-level optimization and model predictive control is proposed to solve the conflict between the computational cost and control accuracy of the flapping-wing micro aerial vehicle. First, a quasi-steady model is established to evaluate the aerodynamic force...

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Veröffentlicht in:	IEEE access Jg. 12; S. 1
Hauptverfasser:	Zheng, Hongyu, Chen, Wengang, Xie, Fangfang
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Piscataway IEEE 01.01.2024 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Accuracy Aerodynamic forces Aerodynamics Algorithms Atmospheric modeling Computational efficiency Computational modeling Control algorithms Control simulation Control theory Flapping wing vehicle Flapping wings Force Kinematics Micro air vehicles (MAV) Model predictive control Multi-level optimization Optimization Optimization models PD control PI control Predictive control Predictive models Proportional integral derivative Quasi-steady model Tracking control
ISSN:	2169-3536, 2169-3536
Online-Zugang:	Volltext
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