Controllable Drogue for Automated Aerial Refueling

被引：34

作者：

Williamson, Walton R. ^{[1
]}

Reed, Eric ^{[2
]}

Glenn, Gregory J. ^{[1
]}

Stecko, Stephen M. ^{[3
]}

Musgrave, Jeffrey ^{[4
]}

Takacs, John M. ^{[5
]}

机构：

[1] SySense Inc, Burbank, CA 91502 USA

[2] Arizona Paradrogue Syst, Kingman, AZ 86401 USA

[3] Boeing Co, Adv Aerial Refueling Syst, Boeing Integrated Def Syst, Long Beach, CA 90807 USA

[4] Boeing Phantom Wcrks, Seattle, WA USA

[5] Boeing Integrated Def Syst, Electroopt, Seal Beach, CA 90740 USA

来源：

JOURNAL OF AIRCRAFT | 2010年 / 47卷 / 02期

关键词：

D O I：

10.2514/1.44758

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a new method for controlling and stabilizing an automated refueling drogue. The drogue automatically stabilizes in the presence of winds or receiver forebody effects using drogue canopy manipulation. This paper reports on a characterization and simulation study in which the stability derivatives of a low-speed drogue were calculated based on wind-tunnel data. A simulation was developed using a pendulum-based hose model combined with the aerodynamic drogue model. An active feedback control system is shown to stabilize and control the drogue to hold a commanded steady-state offset.

引用

页码：515 / 527

页数：13

共 11 条

[1] *CRC, 2003, CRC HDB MECH ENG
[2] DRYDEN HL, 1961, TURBULENCE CLASSIC P
[3] DYNAMIC ANALYSIS OF AN IN-FLIGHT REFUELING SYSTEM
EICHLER, J
[J]. JOURNAL OF AIRCRAFT, 1978, 15 (05): : 311 - 318
[4] ELLSWORTH JA, 1978, E23027 TR US DEP NAV
[5] HANSEN JL, 2005, TM2005212859 NASA DR
[6] Knacke T.W., 1992, PARACHUTE RECOVERY S
[7] Ribbens W B, 2007, 25 AIAA APPL AER C M, P2007
[8] RO K, 2006, 44 AIAA AER SCI M EX
[9] Vassberg J. C., 2005, 23 AIAA APPL AER C J
[10] Elastodynamic analysis of aerial refueling hose using curved beam element
Zhu, ZH
Meguid, SA
[J]. AIAA JOURNAL, 2006, 44 (06) : 1317 - 1324

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