Nonlinear Model Identification Methodology for Small, Fixed-Wing, Unmanned Aircraft-Reference-Cited by-同舟云学术

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Nonlinear Model Identification Methodology for Small, Fixed-Wing, Unmanned Aircraft

Published:2019-05 Issue:3 Volume:56 Page:1056-1067
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Simmons Benjamin M.¹,McClelland Hunter G.¹,Woolsey Craig A.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Funder

Division of Computer and Network Systems

Division of Atmospheric and Geospace Sciences

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.C035160

Reference19 articles.

1. Output-Error Method

2. Development and Modeling of a Low-Cost Unmanned Aerial Vehicle Research Platform

3. Two-Step System Identification and Trajectory Tracking Control of a Small Fixed-Wing UAV

4. System Identification for Small, Low-Cost, Fixed-Wing Unmanned Aircraft

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4. Low-Cost Differential Flatness Identification for Trajectory Planning and Tracking of Small Fixed-Wing UAVs in Dense Environments;2024 International Conference on Unmanned Aircraft Systems (ICUAS);2024-06-04

5. Angular acceleration estimation and aerodynamic parameter identification based on angular velocity equivalent model;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-05-13

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