Dynamic modeling of a hose-drogue aerial refueling system and integral sliding mode backstepping control for the hose whipping phenomenon
Dynamic modeling of a hose-drogue aerial refueling system（HDARS） and an integral sliding mode backstepping controller design for the hose whipping phenomenon（HWP） during probe-drogue coupling are studied. Firstly, a dynamic model of the variable-length hose-drogue assembly is built for the sake of e...
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| Published in | Chinese journal of aeronautics Vol. 27; no. 4; pp. 930 - 946 |
|---|---|
| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Elsevier Ltd
01.08.2014
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1000-9361 2588-9230 |
| DOI | 10.1016/j.cja.2014.06.010 |
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| Abstract | Dynamic modeling of a hose-drogue aerial refueling system（HDARS） and an integral sliding mode backstepping controller design for the hose whipping phenomenon（HWP） during probe-drogue coupling are studied. Firstly, a dynamic model of the variable-length hose-drogue assembly is built for the sake of exploiting suppression methods for the whipping phenomenon.Based on the lumped parameter method, the hose is modeled by a series of variable-length links connected with frictionless joints. A set of iterative equations of the hose＇s three-dimensional motion is derived subject to hose reeling in/out, tanker motion, gravity, and aerodynamic loads accounting for the effects of steady wind, atmospheric turbulence, and tanker wake. Secondly,relying on a permanent magnet synchronous motor and high-precision position sensors, a new active control strategy for the HWP on the basis of the relative position between the tanker and the receiver is proposed. Considering the strict-feedback configuration of the permanent magnet synchronous motor, a rotor position control law based on the backstepping method is designed to insure global stability. An integral of the rotor position error and an exponential sliding mode reaching law of the current errors are applied to enhance control accuracy and robustness. Finally,the simulation results show the effectiveness of the proposed model and control laws. |
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| AbstractList | Dynamic modeling of a hose-drogue aerial refueling system（HDARS） and an integral sliding mode backstepping controller design for the hose whipping phenomenon（HWP） during probe-drogue coupling are studied. Firstly, a dynamic model of the variable-length hose-drogue assembly is built for the sake of exploiting suppression methods for the whipping phenomenon.Based on the lumped parameter method, the hose is modeled by a series of variable-length links connected with frictionless joints. A set of iterative equations of the hose＇s three-dimensional motion is derived subject to hose reeling in/out, tanker motion, gravity, and aerodynamic loads accounting for the effects of steady wind, atmospheric turbulence, and tanker wake. Secondly,relying on a permanent magnet synchronous motor and high-precision position sensors, a new active control strategy for the HWP on the basis of the relative position between the tanker and the receiver is proposed. Considering the strict-feedback configuration of the permanent magnet synchronous motor, a rotor position control law based on the backstepping method is designed to insure global stability. An integral of the rotor position error and an exponential sliding mode reaching law of the current errors are applied to enhance control accuracy and robustness. Finally,the simulation results show the effectiveness of the proposed model and control laws. Dynamic modeling of a hose-drogue aerial refueling system (HDARS) and an integral sliding mode backstepping controller design for the hose whipping phenomenon (HWP) during probe-drogue coupling are studied. Firstly, a dynamic model of the variable-length hose-drogue assembly is built for the sake of exploiting suppression methods for the whipping phenomenon. Based on the lumped parameter method, the hose is modeled by a series of variable-length links connected with frictionless joints. A set of iterative equations of the hose's three-dimensional motion is derived subject to hose reeling in/out, tanker motion, gravity, and aerodynamic loads accounting for the effects of steady wind, atmospheric turbulence, and tanker wake. Secondly, relying on a permanent magnet synchronous motor and high-precision position sensors, a new active control strategy for the HWP on the basis of the relative position between the tanker and the receiver is proposed. Considering the strict-feedback configuration of the permanent magnet synchronous motor, a rotor position control law based on the backstepping method is designed to insure global stability. An integral of the rotor position error and an exponential sliding mode reaching law of the current errors are applied to enhance control accuracy and robustness. Finally, the simulation results show the effectiveness of the proposed model and control laws. |
| Author | Wang Haitao Dong Xinmin Xue Jianping Liu Jiaolong |
| AuthorAffiliation | Aeronautics and Astronautics Engineering College, Air Force Engineering University,Xi＇an 710038, China |
| Author_xml | – sequence: 1 givenname: Haitao surname: Wang fullname: Wang, Haitao email: wanghaitao198638@163.com – sequence: 2 givenname: Xinmin surname: Dong fullname: Dong, Xinmin email: dongxinmin@139.com – sequence: 3 givenname: Jianping surname: Xue fullname: Xue, Jianping email: xiankgy@163.com – sequence: 4 givenname: Jiaolong surname: Liu fullname: Liu, Jiaolong email: kgd_ljl@163.com |
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| Keywords | Backstepping Hose drogue assembly Whipping phenomenon Permanent magnet synchronous motor Sliding mode Aerial refueling |
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| Notes | Aerial refueling;Backstepping;Hose drogue assembly;Permanent magnet synchronous motor;Sliding mode;Whipping phenomenon Dynamic modeling of a hose-drogue aerial refueling system（HDARS） and an integral sliding mode backstepping controller design for the hose whipping phenomenon（HWP） during probe-drogue coupling are studied. Firstly, a dynamic model of the variable-length hose-drogue assembly is built for the sake of exploiting suppression methods for the whipping phenomenon.Based on the lumped parameter method, the hose is modeled by a series of variable-length links connected with frictionless joints. A set of iterative equations of the hose＇s three-dimensional motion is derived subject to hose reeling in/out, tanker motion, gravity, and aerodynamic loads accounting for the effects of steady wind, atmospheric turbulence, and tanker wake. Secondly,relying on a permanent magnet synchronous motor and high-precision position sensors, a new active control strategy for the HWP on the basis of the relative position between the tanker and the receiver is proposed. Considering the strict-feedback configuration of the permanent magnet synchronous motor, a rotor position control law based on the backstepping method is designed to insure global stability. An integral of the rotor position error and an exponential sliding mode reaching law of the current errors are applied to enhance control accuracy and robustness. Finally,the simulation results show the effectiveness of the proposed model and control laws. 11-1732/V ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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| References_xml | – reference: ; 2002. – reference: Vassberg JC, Yeh DT, Blair AJ, Evert JM. Dynamic characteristics of a KC-10 wing-pod refueling hose by numerical simulation. – reference: Alden RE, Vennero GG, inventor; Whittaker Controls Inc., assignee. Aerial refueling system. United States patent US 5141178. 1992 Aug 25. – reference: Vachon MJ, Ray RJ. Calculated drag of an aerial refueling assembly through airplane performance analysis. – reference: Bartov A, inventor. Method for engaging a probe and drogue for aerial refueling. United States patent US 6786455B1. 2004 Sep 7. – reference: Vassberg JC, Yeh DT, Blair AJ, Evert JM. 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| Snippet | Dynamic modeling of a hose-drogue aerial refueling system（HDARS） and an integral sliding mode backstepping controller design for the hose whipping... Dynamic modeling of a hose-drogue aerial refueling system (HDARS) and an integral sliding mode backstepping controller design for the hose whipping phenomenon... |
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| StartPage | 930 |
| SubjectTerms | Aerial refueling Backstepping Dynamical systems Dynamics Hose drogue assembly Hoses Integrals Law Permanent magnet synchronous motor Permanent magnets Sliding mode Tankers Whipping phenomenon 动态建模 反推控制 永磁同步电机 滑模 积分 空中加油系统 软管 锥套 |
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| Title | Dynamic modeling of a hose-drogue aerial refueling system and integral sliding mode backstepping control for the hose whipping phenomenon |
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