000075726 001__ 75726
000075726 005__ 20200221144242.0
000075726 0247_ $$2doi$$a10.2514/1.G001598
000075726 0248_ $$2sideral$$a108325
000075726 037__ $$aART-2016-108325
000075726 041__ $$aeng
000075726 100__ $$0(orcid)0000-0001-9744-5732$$aAvendaño, M.
000075726 245__ $$aAn algebraic approach to the minimum-cost multi-impulse orbit transfer problem
000075726 260__ $$c2016
000075726 5060_ $$aAccess copy available to the general public$$fUnrestricted
000075726 5203_ $$aA purely algebraic formulation (i.e., polynomial equations only) of the minimum-cost multi-impulse orbit-transfer problem without time constraints is presented, while keeping all the variables with a precise physical meaning. General algebraic techniques are applied to solve these equations (resultants, Gröbner bases, etc.) in several situations of practical interest of different degrees of generality. For instance, a proof of the optimality of the Hohmann transfer for the minimum-fuel two-impulse circular-to-circular orbit-transfer problem is provided. Finally, a general formula is also provided for the optimal two-impulse in-plane transfer between two rotated elliptical orbits under a mild symmetry assumption on the two points where the impulses are applied (which, it is conjectured, can be removed).
000075726 536__ $$9info:eu-repo/grantAgreement/ES/DGA/E15$$9info:eu-repo/grantAgreement/ES/MICINN/MTM2013-45710-C2-1-P$$9info:eu-repo/grantAgreement/ES/MINECO/MTM2011-22621$$9info:eu-repo/grantAgreement/ES/MINECO/MTM2014-52197-P$$9info:eu-repo/grantAgreement/ES/MINECO/2013-44217-R$$9info:eu-repo/grantAgreement/ES/UZ/CUD2013-15
000075726 540__ $$9info:eu-repo/semantics/openAccess$$aAll rights reserved$$uhttp://www.europeana.eu/rights/rr-f/
000075726 590__ $$a1.856$$b2016
000075726 591__ $$aENGINEERING, AEROSPACE$$b5 / 31 = 0.161$$c2016$$dQ1$$eT1
000075726 591__ $$aINSTRUMENTS & INSTRUMENTATION$$b22 / 58 = 0.379$$c2016$$dQ2$$eT2
000075726 592__ $$a1.181$$b2016
000075726 593__ $$aAerospace Engineering$$c2016$$dQ1
000075726 593__ $$aApplied Mathematics$$c2016$$dQ1
000075726 593__ $$aControl and Systems Engineering$$c2016$$dQ1
000075726 593__ $$aElectrical and Electronic Engineering$$c2016$$dQ1
000075726 593__ $$aSpace and Planetary Science$$c2016$$dQ2
000075726 655_4 $$ainfo:eu-repo/semantics/article$$vinfo:eu-repo/semantics/submittedVersion
000075726 700__ $$0(orcid)0000-0002-6359-5246$$aMartín-Molina, V.
000075726 700__ $$0(orcid)0000-0002-6559-4722$$aMartin Morales, Jorge
000075726 700__ $$0(orcid)0000-0002-6635-8780$$aOrtigas-Galindo, J.$$uUniversidad de Zaragoza
000075726 7102_ $$12006$$2015$$aUniversidad de Zaragoza$$bDpto. Matemáticas$$cÁrea Análisis Matemático
000075726 773__ $$g39, 8 (2016), 1734-1743$$pJ. guid. control dyn.$$tJOURNAL OF GUIDANCE CONTROL AND DYNAMICS$$x0731-5090
000075726 8564_ $$s763868$$uhttps://zaguan.unizar.es/record/75726/files/texto_completo.pdf$$yPreprint
000075726 8564_ $$s88887$$uhttps://zaguan.unizar.es/record/75726/files/texto_completo.jpg?subformat=icon$$xicon$$yPreprint
000075726 909CO $$ooai:zaguan.unizar.es:75726$$particulos$$pdriver
000075726 951__ $$a2020-02-21-13:22:25
000075726 980__ $$aARTICLE