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contributor authorP. Seiler
contributor authorA. Pant
contributor authorJ. K. Hedrick
date accessioned2017-05-09T00:12:29Z
date available2017-05-09T00:12:29Z
date copyrightDecember, 2004
date issued2004
identifier issn0022-0434
identifier otherJDSMAA-26336#873_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/129727
description abstractFlying in formation improves aerodynamic efficiency and, consequently, leads to an energy savings. One strategy for formation control is to follow the preceding vehicle. Many researchers have shown through simulation results and analysis of specific control laws that this strategy leads to amplification of disturbances as they propagate through the formation. This effect is known as string instability. In this paper, we show that string instability is due to a fundamental constraint on coupled feedback loops. The tradeoffs imposed by this constraint imply that predecessor following is an inherently poor strategy for formation flight control. Finally, we present two examples that demonstrate the theoretical results.
publisherThe American Society of Mechanical Engineers (ASME)
titleString Instabilities in Formation Flight: Limitations Due to Integral Constraints
typeJournal Paper
journal volume126
journal issue4
journal titleJournal of Dynamic Systems, Measurement, and Control
identifier doi10.1115/1.1858444
journal fristpage873
journal lastpage879
identifier eissn1528-9028
keywordsString
keywordsVehicles
keywordsErrors
keywordsFeedback
keywordsFlight
keywordsDynamics (Mechanics)
keywordsAircraft
keywordsTransfer functions
keywordsControl equipment AND Helicopters
treeJournal of Dynamic Systems, Measurement, and Control:;2004:;volume( 126 ):;issue: 004
contenttypeFulltext


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