Chinese Space Science and Technology ›› 2012, Vol. 32 ›› Issue (2): 77-83.doi: 10.3780/j.issn.1000-758X.2012.02.012
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ZHANG Wei1, FENG Xiao-Hui2, DENG Zhong-Min1
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Abstract: Basedontheline-of-sightmeasurement,acooperativecontrolmethodforleaderlessformationflightispresented.Line-of-sightvectormeasurementisgeneratedwheneachsatelliteinaformationtracksitsneighboringspacecraft.Thefirstmemberoftheformationtracksthedesiredorbitaccordingtothecommandfromahighlevelcontroller.Achainformationisgenerated.Distancesbetweenline-of-sightmeasurementsaretakenasfeedbackoftheformationcontroller.Therelativeperturbationequationsareprovidedtomakesurethatmodelinguncertaintiesandperturbationsareconsideredinthecontrolstrategy.Cyclicformationcontrolisperformedviaslidingmodecontroller.Simulationresultsshowthattheproposedcontrolmethodcanbeusedforsatelliteformationmaintenanceandmaneuver.
Key words: Spacecraft formation, Line-of-sight measurement, Coordinated control, Sliding mode control, Microsatellite
ZHANG Wei, FENG Xiao-Hui, DENG Zhong-Min. CoordinatedManeuverofSpacecraftFormationBasedonLine-of-sightMeasurement [J]. Chinese Space Science and Technology, 2012, 32(2): 77-83.
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