Design of flying boom controller before and after docking

Huazi Cao; Lixin Wang; Ting Yue

doi:10.1109/CGNCC.2016.7828989

Design of flying boom controller before and after docking

Huazi Cao
, Lixin Wang
, Ting Yue

School of Aeronautic Science and Engineering

Beihang University

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

5 Scopus citations

Abstract

An increasing interest over the last decades in developing aerial boom refueling technology has prompted research into controller design of flying boom. During air-to-air refueling, there are two task for flying boom controller divided by docking respectively: attitude control and unloading control. Under some assumptions, the dynamic models before and after docking are built. Based on the dynamic model before docking, the sliding mode disturbance observer based back-stepping adaptive controller is used in attitude control after dividing the dynamic model into two subsystems. Then, the unloading controller is designed to eliminate the radial constraint force. After designing, the asymptotical stability of unload controller is proved by Barbalat's lemma. The effectiveness and adaptability is shown in the results of simulations with complex circumstance of flying boom.

Original language	English
Title of host publication	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	1375-1380
Number of pages	6
ISBN (Electronic)	9781467383189
DOIs	https://doi.org/10.1109/CGNCC.2016.7828989
State	Published - 20 Jan 2017
Event	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, China Duration: 12 Aug 2016 → 14 Aug 2016

Publication series

Name	CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

Conference

Conference	7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
Country/Territory	China
City	Nanjing, Jiangsu
Period	12/08/16 → 14/08/16

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10.1109/CGNCC.2016.7828989

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Cao, H., Wang, L., & Yue, T. (2017). Design of flying boom controller before and after docking. In CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference (pp. 1375-1380). Article 7828989 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CGNCC.2016.7828989

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title = "Design of flying boom controller before and after docking",

abstract = "An increasing interest over the last decades in developing aerial boom refueling technology has prompted research into controller design of flying boom. During air-to-air refueling, there are two task for flying boom controller divided by docking respectively: attitude control and unloading control. Under some assumptions, the dynamic models before and after docking are built. Based on the dynamic model before docking, the sliding mode disturbance observer based back-stepping adaptive controller is used in attitude control after dividing the dynamic model into two subsystems. Then, the unloading controller is designed to eliminate the radial constraint force. After designing, the asymptotical stability of unload controller is proved by Barbalat's lemma. The effectiveness and adaptability is shown in the results of simulations with complex circumstance of flying boom.",

author = "Huazi Cao and Lixin Wang and Ting Yue",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 ; Conference date: 12-08-2016 Through 14-08-2016",

year = "2017",

month = jan,

day = "20",

doi = "10.1109/CGNCC.2016.7828989",

language = "英语",

series = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

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booktitle = "CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference",

address = "美国",

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Cao, H, Wang, L & Yue, T 2017, Design of flying boom controller before and after docking. in CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference., 7828989, CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference, Institute of Electrical and Electronics Engineers Inc., pp. 1375-1380, 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016, Nanjing, Jiangsu, China, 12/08/16. https://doi.org/10.1109/CGNCC.2016.7828989

Design of flying boom controller before and after docking. / Cao, Huazi; Wang, Lixin ; Yue, Ting.
CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference. Institute of Electrical and Electronics Engineers Inc., 2017. p. 1375-1380 7828989 (CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference).

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

TY - GEN

T1 - Design of flying boom controller before and after docking

AU - Cao, Huazi

AU - Wang, Lixin

AU - Yue, Ting

PY - 2017/1/20

Y1 - 2017/1/20

N2 - An increasing interest over the last decades in developing aerial boom refueling technology has prompted research into controller design of flying boom. During air-to-air refueling, there are two task for flying boom controller divided by docking respectively: attitude control and unloading control. Under some assumptions, the dynamic models before and after docking are built. Based on the dynamic model before docking, the sliding mode disturbance observer based back-stepping adaptive controller is used in attitude control after dividing the dynamic model into two subsystems. Then, the unloading controller is designed to eliminate the radial constraint force. After designing, the asymptotical stability of unload controller is proved by Barbalat's lemma. The effectiveness and adaptability is shown in the results of simulations with complex circumstance of flying boom.

AB - An increasing interest over the last decades in developing aerial boom refueling technology has prompted research into controller design of flying boom. During air-to-air refueling, there are two task for flying boom controller divided by docking respectively: attitude control and unloading control. Under some assumptions, the dynamic models before and after docking are built. Based on the dynamic model before docking, the sliding mode disturbance observer based back-stepping adaptive controller is used in attitude control after dividing the dynamic model into two subsystems. Then, the unloading controller is designed to eliminate the radial constraint force. After designing, the asymptotical stability of unload controller is proved by Barbalat's lemma. The effectiveness and adaptability is shown in the results of simulations with complex circumstance of flying boom.

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DO - 10.1109/CGNCC.2016.7828989

M3 - 会议稿件

AN - SCOPUS:85015178407

T3 - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

SP - 1375

EP - 1380

BT - CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016

Y2 - 12 August 2016 through 14 August 2016

ER -

Design of flying boom controller before and after docking

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