摘要
Thisletterproposesamethodfordesigningaspecificformationofsatelliteswheretheflyingmotiononlyexistsinacircleorbitplaneofthereferencesatellite,whichmeansthattheorbiteccen-tricityiszero.ThismethodcombinestheHillequation,theKeplerequation,andthegeometricalmeaningoforbitelements.Itcreatestheredundancyconditiontosimplifythededucingprocess,utilizesmultipleconditionstosolvetheorbitelementsforthesatelliteformation,andobtainstheanalyticalrelationshipoftheorbitelementsfortheformationsatelliteswiththeformationparametersandtheorbitelementsofthereferencesatellite.Usingtheseformulations,theorbitelementsandformationparametersfortheformationsatellitescanbesolvedforthegivenorbitelementsofthereferencesatellite.Theletterdescribestheproposeddouble-ellipseformationforbothGMTIandInSAR,andthevalidityoftheformationisdemonstratedviasimulation.
出版日期
2007年06月16日（中国期刊网平台首次上网日期，不代表论文的发表时间）
