Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft

Yang Wang; Changle Xiang; Yue Ma; Bin Xu

doi:10.1109/CGNCC.2014.7007242

Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft

Yang Wang^*, Changle Xiang, Yue Ma, Bin Xu

^*Corresponding author for this work

School of Mechanical Engineering

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

10 Citations (Scopus)

Abstract

Force and torque generation mechanisms for an unconventional tandem ducted fan aircraft are investigated. Numerical techniques are implemented to obtain quasi-steady thrust, numerical integration of nonlinear equations of motion and trim iteration process, respectively. The comprehensive nonlinear model is derived and simplified to linear approximations at different flight conditions for stability and input-output controllability analysis. Specifically, modal analysis is performed for the vehicle at hover and forward flight. Quantitative input-output controllability analysis is then applied to our plant to find out the fundamental controller-independent limitations and capture what performance can be expected.

Original language	English
Title of host publication	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	255-261
Number of pages	7
ISBN (Electronic)	9781479946990
DOIs	https://doi.org/10.1109/CGNCC.2014.7007242
Publication status	Published - 12 Jan 2015
Event	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, China Duration: 8 Aug 2014 → 10 Aug 2014

Publication series

Name	2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

Conference

Conference	6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
Country/Territory	China
City	Yantai
Period	8/08/14 → 10/08/14

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10.1109/CGNCC.2014.7007242

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Wang, Y., Xiang, C., Ma, Y., & Xu, B. (2015). Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft. In 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 (pp. 255-261). Article 7007242 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2014.7007242

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title = "Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft",

abstract = "Force and torque generation mechanisms for an unconventional tandem ducted fan aircraft are investigated. Numerical techniques are implemented to obtain quasi-steady thrust, numerical integration of nonlinear equations of motion and trim iteration process, respectively. The comprehensive nonlinear model is derived and simplified to linear approximations at different flight conditions for stability and input-output controllability analysis. Specifically, modal analysis is performed for the vehicle at hover and forward flight. Quantitative input-output controllability analysis is then applied to our plant to find out the fundamental controller-independent limitations and capture what performance can be expected.",

author = "Yang Wang and Changle Xiang and Yue Ma and Bin Xu",

note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 ; Conference date: 08-08-2014 Through 10-08-2014",

year = "2015",

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day = "12",

doi = "10.1109/CGNCC.2014.7007242",

language = "English",

series = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",

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Wang, Y, Xiang, C, Ma, Y & Xu, B 2015, Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft. in 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014., 7007242, 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Institute of Electrical and Electronics Engineers Inc., pp. 255-261, 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014, Yantai, China, 8/08/14. https://doi.org/10.1109/CGNCC.2014.7007242

Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft. / Wang, Yang; Xiang, Changle; Ma, Yue et al.
2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc., 2015. p. 255-261 7007242 (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Xiang, Changle

AU - Ma, Yue

AU - Xu, Bin

PY - 2015/1/12

Y1 - 2015/1/12

N2 - Force and torque generation mechanisms for an unconventional tandem ducted fan aircraft are investigated. Numerical techniques are implemented to obtain quasi-steady thrust, numerical integration of nonlinear equations of motion and trim iteration process, respectively. The comprehensive nonlinear model is derived and simplified to linear approximations at different flight conditions for stability and input-output controllability analysis. Specifically, modal analysis is performed for the vehicle at hover and forward flight. Quantitative input-output controllability analysis is then applied to our plant to find out the fundamental controller-independent limitations and capture what performance can be expected.

AB - Force and torque generation mechanisms for an unconventional tandem ducted fan aircraft are investigated. Numerical techniques are implemented to obtain quasi-steady thrust, numerical integration of nonlinear equations of motion and trim iteration process, respectively. The comprehensive nonlinear model is derived and simplified to linear approximations at different flight conditions for stability and input-output controllability analysis. Specifically, modal analysis is performed for the vehicle at hover and forward flight. Quantitative input-output controllability analysis is then applied to our plant to find out the fundamental controller-independent limitations and capture what performance can be expected.

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BT - 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

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Wang Y, Xiang C, Ma Y , Xu B. Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft. In 2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014. Institute of Electrical and Electronics Engineers Inc. 2015. p. 255-261. 7007242. (2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014). doi: 10.1109/CGNCC.2014.7007242

Comprehensive nonlinear modeling and simulation analysis of a tandem ducted fan aircraft

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