000101198 001__ 101198
000101198 005__ 20230126102840.0
000101198 0247_ $$2doi$$a10.2514/1.G004300
000101198 0248_ $$2sideral$$a123043
000101198 037__ $$aART-2019-123043
000101198 041__ $$aeng
000101198 100__ $$0(orcid)0000-0002-3312-5710$$aCalvo, M.$$uUniversidad de Zaragoza
000101198 245__ $$aApproximate trigonometric series expansions of some bounded solutions in the Tsien problem
000101198 260__ $$c2019
000101198 5060_ $$aAccess copy available to the general public$$fUnrestricted
000101198 5203_ $$aINTHE last decades, studies on the dynamics of a spacecraft that is moving in the gravitational field of a celestial body and subjected to some low-thrust propulsion system have attracted the attention of many researchers in astrodynamics.
Here, we consider a particular case, the so-called Tsien problem [1], in which the spacecraft moves in a circular Keplerian orbit (often referred to as the parking orbit), and after a given time t0 0, it is subjected to a constant outward radial acceleration.
By using the integrals of energy and angular momentum, this problem can be reduced to a two-dimensional scenario. Denoting by r and ? the polar coordinates that give the position of the spacecraft in the plane of the orbit [1], the differential equations that define their motion are ...
000101198 536__ $$9info:eu-repo/grantAgreement/ES/DGA-FEDER/E41-17R$$9info:eu-repo/grantAgreement/ES/DGA-FSE/E24-17R$$9info:eu-repo/grantAgreement/ES/MINECO/ESP2017-87113-R$$9info:eu-repo/grantAgreement/ES/MINECO/MTM2016-77735-C3-1-P
000101198 540__ $$9info:eu-repo/semantics/openAccess$$aAll rights reserved$$uhttp://www.europeana.eu/rights/rr-f/
000101198 590__ $$a2.692$$b2019
000101198 591__ $$aENGINEERING, AEROSPACE$$b6 / 31 = 0.194$$c2019$$dQ1$$eT1
000101198 591__ $$aINSTRUMENTS & INSTRUMENTATION$$b21 / 64 = 0.328$$c2019$$dQ2$$eT1
000101198 592__ $$a1.573$$b2019
000101198 593__ $$aAerospace Engineering$$c2019$$dQ1
000101198 593__ $$aApplied Mathematics$$c2019$$dQ1
000101198 593__ $$aSpace and Planetary Science$$c2019$$dQ1
000101198 593__ $$aElectrical and Electronic Engineering$$c2019$$dQ1
000101198 593__ $$aControl and Systems Engineering$$c2019$$dQ1
000101198 655_4 $$ainfo:eu-repo/semantics/article$$vinfo:eu-repo/semantics/acceptedVersion
000101198 700__ $$0(orcid)0000-0001-6120-4427$$aMontijano, J.I.$$uUniversidad de Zaragoza
000101198 700__ $$0(orcid)0000-0002-4238-3228$$aRández, L.$$uUniversidad de Zaragoza
000101198 700__ $$0(orcid)0000-0001-5208-4494$$aElipe, A.$$uUniversidad de Zaragoza
000101198 7102_ $$12005$$2595$$aUniversidad de Zaragoza$$bDpto. Matemática Aplicada$$cÁrea Matemática Aplicada
000101198 773__ $$g42, 10 (2019), 2325-2330$$pJ. guid. control dyn.$$tJOURNAL OF GUIDANCE CONTROL AND DYNAMICS$$x0731-5090
000101198 8564_ $$s625519$$uhttps://zaguan.unizar.es/record/101198/files/texto_completo.pdf$$yPostprint
000101198 8564_ $$s1109852$$uhttps://zaguan.unizar.es/record/101198/files/texto_completo.jpg?subformat=icon$$xicon$$yPostprint
000101198 909CO $$ooai:zaguan.unizar.es:101198$$particulos$$pdriver
000101198 951__ $$a2023-01-26-09:56:52
000101198 980__ $$aARTICLE