Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach

Duc H Nguyen; Mark H Lowenberg; Simon A Neild; Tom S Richardson

doi:10.2514/1.G005866

Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach

Duc H Nguyen, Mark H Lowenberg , Simon A Neild, Tom S Richardson

Research output: Contribution to journal › Article (Academic Journal) › peer-review

1 Citation (Scopus)

119 Downloads (Pure)

Abstract

[No Abstract]

Original language	English
Pages (from-to)	1692-1699
Number of pages	8
Journal	Journal of Guidance, Control, and Dynamics
Volume	44
Issue number	9
Early online date	10 May 2021
DOIs	https://doi.org/10.2514/1.G005866
Publication status	Published - 2021

Bibliographical note

Funding Information:
The first author is partially funded by the University of Bristol’s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged.

Funding Information:
The first author is partially funded by the University of Bristol?s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged.

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10.2514/1.G005866

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This is the author accepted manuscript (AAM). The final published version (version of record) is available online via American Institute of Aeronautics and Astronautics at https://arc.aiaa.org/doi/pdf/10.2514/1.G005866 . Please refer to any applicable terms of use of the publisher.
Accepted author manuscript, 1.42 MB

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Extending Nonlinear Frequency Analysis to Flight Dynamics and Control Problems
Nguyen, D. H. (Author), Neild, S. (Supervisor) & Lowenberg, M. (Supervisor), 2 Dec 2021
Student thesis: Doctoral Thesis › Doctor of Philosophy (PhD)

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title = "Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach",

abstract = "[No Abstract]",

author = "Nguyen, {Duc H} and Lowenberg, {Mark H} and Neild, {Simon A} and Richardson, {Tom S}",

note = "Funding Information: The first author is partially funded by the University of Bristol{\textquoteright}s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged. Funding Information: The first author is partially funded by the University of Bristol?s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged.",

year = "2021",

doi = "10.2514/1.G005866",

language = "English",

volume = "44",

pages = "1692--1699",

journal = "Journal of Guidance, Control, and Dynamics",

issn = "0731-5090",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

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TY - JOUR

T1 - Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach

AU - Nguyen, Duc H

AU - Lowenberg , Mark H

AU - Neild, Simon A

AU - Richardson, Tom S

N1 - Funding Information: The first author is partially funded by the University of Bristol’s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged. Funding Information: The first author is partially funded by the University of Bristol?s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged.

PY - 2021

Y1 - 2021

N2 - [No Abstract]

AB - [No Abstract]

U2 - 10.2514/1.G005866

DO - 10.2514/1.G005866

M3 - Article (Academic Journal)

SN - 0731-5090

VL - 44

SP - 1692

EP - 1699

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 9

ER -

Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach

Abstract

Bibliographical note

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Student theses

Extending Nonlinear Frequency Analysis to Flight Dynamics and Control Problems

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