000130399 001__ 130399 000130399 005__ 20240125162929.0 000130399 0247_ $$2doi$$a10.2514/1.38350 000130399 0248_ $$2sideral$$a63478 000130399 037__ $$aART-2009-63478 000130399 041__ $$aeng 000130399 100__ $$0(orcid)0000-0002-5692-5876$$aAbad, A.$$uUniversidad de Zaragoza 000130399 245__ $$aAnalytical Model to Find Frozen Orbits for a Lunar Orbiter 000130399 260__ $$c2009 000130399 5060_ $$aAccess copy available to the general public$$fUnrestricted 000130399 5203_ $$aAnalytical theories based on Lie-Deprit transforms are used to obtain families of periodic orbits for the problem of an orbiter around the moon. Low and moderately high orbit models are analyzed. Equilibria of the normalized equations of motion provide the representation of a global portrait of families of frozen orbits depending on values of the inclination, eccentricity, and semimajor axis. By means of the inverse transformation it is possible to refine the initial conditions for frozen orbits of a simplified model, and these initial conditions may be used as starters of numerical continuation methods when more complex models are considered. 000130399 536__ $$9info:eu-repo/grantAgreement/ES/MICYT/ESP2005-07107$$9info:eu-repo/grantAgreement/ES/MICYT/MTM2006-06961 000130399 540__ $$9info:eu-repo/semantics/openAccess$$aAll rights reserved$$uhttp://www.europeana.eu/rights/rr-f/ 000130399 590__ $$a1.031$$b2009 000130399 591__ $$aENGINEERING, AEROSPACE$$b4 / 26 = 0.154$$c2009$$dQ1$$eT1 000130399 591__ $$aINSTRUMENTS & INSTRUMENTATION$$b26 / 57 = 0.456$$c2009$$dQ2$$eT2 000130399 655_4 $$ainfo:eu-repo/semantics/article$$vinfo:eu-repo/semantics/acceptedVersion 000130399 700__ $$0(orcid)0000-0001-5208-4494$$aElipe, A.$$uUniversidad de Zaragoza 000130399 700__ $$0(orcid)0000-0003-4859-7224$$aTresaco, E.$$uUniversidad de Zaragoza 000130399 7102_ $$12005$$2595$$aUniversidad de Zaragoza$$bDpto. Matemática Aplicada$$cÁrea Matemática Aplicada 000130399 7102_ $$12004$$2398$$aUniversidad de Zaragoza$$bDpto. Física Teórica$$cÁrea Física de la Tierra 000130399 773__ $$g32, 3 (2009), 888-898$$pJ. guid. control dyn.$$tJOURNAL OF GUIDANCE CONTROL AND DYNAMICS$$x0731-5090 000130399 8564_ $$s4233209$$uhttps://zaguan.unizar.es/record/130399/files/texto_completo.pdf$$yPostprint 000130399 8564_ $$s2318703$$uhttps://zaguan.unizar.es/record/130399/files/texto_completo.jpg?subformat=icon$$xicon$$yPostprint 000130399 909CO $$ooai:zaguan.unizar.es:130399$$particulos$$pdriver 000130399 951__ $$a2024-01-25-15:07:30 000130399 980__ $$aARTICLE