An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft

Weifang Shuang; Shaojie Zhang; Xue Wu; Erik-Jan van Kampen; Qiping Chu

doi:10.2514/6.2017-1253

An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft

Weifang Shuang, Shaojie Zhang, Xue Wu, Erik-Jan van Kampen, Qiping Chu

Control & Simulation

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

9 Citations (Scopus)

111 Downloads (Pure)

Abstract

Original language	English
Title of host publication	AIAA Guidance, Navigation, and Control Conference, 2017
Subtitle of host publication	January 9-13, Grapevine, TX
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Number of pages	11
ISBN (Electronic)	978-1-62410-450-3
DOIs	https://doi.org/10.2514/6.2017-1253
Publication status	Published - 2017
Event	AIAA Guidance, Navigation, and Control Conference, 2017 - Grapevine, United States Duration: 9 Jan 2017 → 13 Jan 2017 https://doi.org/10.2514/MGNC17

Conference

Conference	AIAA Guidance, Navigation, and Control Conference, 2017
Country/Territory	United States
City	Grapevine
Period	9/01/17 → 13/01/17
Internet address	https://doi.org/10.2514/MGNC17

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An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing AircraftAccepted author manuscript, 461 KB

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Shuang, W., Zhang, S., Wu, X., van Kampen, E.-J., & Chu, Q. (2017). An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft. In AIAA Guidance, Navigation, and Control Conference, 2017: January 9-13, Grapevine, TX Article AIAA 2017-1253 American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2017-1253

@inproceedings{e693923f4907445ba6f95085383bdc0d,

title = "An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft",

author = "Weifang Shuang and Shaojie Zhang and Xue Wu and {van Kampen}, Erik-Jan and Qiping Chu",

year = "2017",

doi = "10.2514/6.2017-1253",

language = "English",

booktitle = "AIAA Guidance, Navigation, and Control Conference, 2017",

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

address = "United States",

note = "AIAA Guidance, Navigation, and Control Conference, 2017 ; Conference date: 09-01-2017 Through 13-01-2017",

url = "https://doi.org/10.2514/MGNC17",

}

Shuang, W, Zhang, S, Wu, X, van Kampen, E-J & Chu, Q 2017, An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft. in AIAA Guidance, Navigation, and Control Conference, 2017: January 9-13, Grapevine, TX., AIAA 2017-1253, American Institute of Aeronautics and Astronautics Inc. (AIAA), AIAA Guidance, Navigation, and Control Conference, 2017, Grapevine, Texas, United States, 9/01/17. https://doi.org/10.2514/6.2017-1253

An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft. / Shuang, Weifang; Zhang, Shaojie; Wu, Xue et al.
AIAA Guidance, Navigation, and Control Conference, 2017: January 9-13, Grapevine, TX. American Institute of Aeronautics and Astronautics Inc. (AIAA), 2017. AIAA 2017-1253.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

T1 - An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft

AU - Shuang, Weifang

AU - Zhang, Shaojie

AU - Wu, Xue

AU - van Kampen, Erik-Jan

AU - Chu, Qiping

PY - 2017

Y1 - 2017

UR - http://resolver.tudelft.nl/uuid:e693923f-4907-445b-a6f9-5085383bdc0d

U2 - 10.2514/6.2017-1253

DO - 10.2514/6.2017-1253

M3 - Conference contribution

BT - AIAA Guidance, Navigation, and Control Conference, 2017

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

T2 - AIAA Guidance, Navigation, and Control Conference, 2017

Y2 - 9 January 2017 through 13 January 2017

ER -

An Anti-windup Fault Tolerant Control Scheme with Guaranteed Transient Performance for Tailless Flying Wing Aircraft

Abstract

Conference

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