Academic Journal

Solution of Low-Thrust Lambert Problem with Perturbative Expansions of Equinoctial Elements

التفاصيل البيبلوغرافية
العنوان: Solution of Low-Thrust Lambert Problem with Perturbative Expansions of Equinoctial Elements
المؤلفون: AVANZINI, Giulio, Palmas, A., Vellutini, E.
المساهمون: Avanzini, Giulio, Palmas, A., Vellutini, E.
سنة النشر: 2015
المجموعة: Università del Salento: CINECA IRIS
مصطلحات موضوعية: Low thrust propulsion, Low thrust trajectory, Lambert problem
الوصف: A method for solving the so-called low-thrust Lambert problem is proposed. After formulating it as a two-point boundary value problem, where initial and final positions are provided in terms of equinoctial variables, a first-order perturbative approach is used for investigating the variation of orbital elements generated by the low-thrust propulsion system, which acts as a perturbing parameter with respect to the zero-order Keplerian motion. An implicit algebraic problem is obtained, which allows for the determination of the low-thrust transfer trajectory that drives the equinoctial parameters from the initial to the final values in a prescribed time. Three test cases are presented, which demonstrate the flexibility of the method for different mission scenarios: an interplanetary transfer from Earth to Mars, a spiral multirevolution transfer from low Earth orbit to the International Space Station, and a maneuver to a highly elliptical orbit with large plane change.
نوع الوثيقة: article in journal/newspaper
وصف الملف: STAMPA
اللغة: English
Relation: info:eu-repo/semantics/altIdentifier/wos/WOS:000361827900006; volume:38; firstpage:1585; lastpage:1601; numberofpages:17; journal:JOURNAL OF GUIDANCE CONTROL AND DYNAMICS; http://hdl.handle.net/11587/395350; info:eu-repo/semantics/altIdentifier/scopus/2-s2.0-84942085231
DOI: 10.2514/1.G001018
الاتاحة: http://hdl.handle.net/11587/395350
https://doi.org/10.2514/1.G001018
http://arc.aiaa.org/doi/10.2514/1.G001018
Rights: info:eu-repo/semantics/openAccess
رقم الانضمام: edsbas.D207607D
قاعدة البيانات: BASE