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在“Elsevier电子期刊”中，命中：94条，耗时：0.0139908 秒

在所有数据库中总计命中：283条

1.Natural periodic orbit-attitude behaviors for rigid bodies in three-body periodic orbits

作者：Davide Guzzetti ; ^{dguzzett@purdue.edu} ; Kathleen C. Howell ^{howell@purdue.edu}

关键词：Multi-body systems ; Three-body problem ; Spacecraft attitude ; Libration points ; Periodic solutions

刊名：Acta Astronautica

出版年：2017

2.Triangular libration points in the R3BP under combined effects of oblateness, radiation and power-law profile

关键词：Restricted three-body problem ; Libration points ; Oblateness ; Power-law density profile

刊名：Advances in Space Research

出版年：2016

3.Numerical investigation of the dynamical environment of 65803 Didymos

作者：L. Dell&rsquo ; Elce^a ; ^{lamberto.dellelce@ulg.ac.be} ; N. Baresi^b ; S.P. Naidu^c ; L.A.M. Benner^c ; D.J. Scheeres^b

关键词：Didymos ; AIDA mission ; Restricted three-body problem

刊名：Advances in Space Research

出版年：2017

4.A note on transfers from LEOs to GEOs visiting libration points of the Sun-Earth CRTBP

作者：Esther Barrabé ; s^a ; ^{barrabes@imae.udg.edu" class="auth_mail" title="E-mail the corresponding author} ; Laura Garcia-Taberner^a ; ^{laura.garcia@imae.udg.edu" class="auth_mail" title="E-mail the corresponding author} ; Gerard Gó ; mez^b ; ^{gerard@maia.ub.es" class="auth_mail" title="E-mail the corresponding author}

关键词：Circular Restricted Three-Body Problem ; Low energy transfer orbits ; LEO orbits ; GEO orbits ; Libration points

刊名：Advances in Space Research

出版年：2016

5.Adaptive surrogate model based multi-objective transfer trajectory optimization between different libration points

作者：Haijun Peng^a ; ^{hjpeng@dlut.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Wei Wang^b

关键词：Surrogate model ; Adaptive sampling ; Multi-objective optimization ; Libration point ; Optimal control ; Invariant manifold

刊名：Advances in Space Research

出版年：2016

6.Adaptive surrogate model-based fast path planning for spacecraft formation reconfiguration on libration point orbits

作者：Haijun Peng^a ; ^{hjpeng@dlut.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Wei Wang^b

关键词：Spacecraft formation reconfiguration ; Fast path planning ; Adaptive surrogate model ; Libration point orbit ; Circular restricted three-body problem

刊名：Aerospace Science and Technology

出版年：2016

7.Identification of new orbits to enable future mission opportunities for the human exploration of the Martian moon Phobos

作者：Mattia Zamaro ; ^{mattia.zamaro@strath.ac.uk" class="auth_mail" title="E-mail the corresponding author}Author Vitae ; James D. Biggs¹ ; ^{james.biggs@strath.ac.uk" class="auth_mail" title="E-mail the corresponding author}Author Vitae

关键词：Phobos ; Mars manned mission ; Libration Point orbits ; Quasi-satellite orbits ; Artificial equilibrium points ; Radiation shielding

刊名：Acta Astronautica

出版年：2016

8.Rapid trajectory design in the Earth-Moon ephemeris system via an interactive catalog of periodic and quasi-periodic orbits

作者：Davide Guzzetti^a ; ^{dguzzett@purdue.edu" class="auth_mail" title="E-mail the corresponding author} ; Natasha Bosanac^a ; ^{nbosanac@purdue.edu" class="auth_mail" title="E-mail the corresponding author} ; Amanda Haapala^a ; ¹ ; ^{amanda.haapala@jhuapl.edu" class="auth_mail" title="E-mail the corresponding author} ; Kathleen C. Howell^a ; ^{howell@purdue.edu" class="auth_mail" title="E-mail the corresponding author} ; David C. Folta^b ; ^{david.c.folta@nasa.gov" class="auth_mail" title="E-mail the corresponding author}

关键词：Multi-body systems ; Three-body problem ; Libration points ; Quasi-periodic solutions ; Periodic solutions

刊名：Acta Astronautica

出版年：2016

9.Recovery of halo orbit missions in case of contingent station-keeping maneuver delay

作者：Maksim Shirobokov ; ^{shmaxg@gmail.com" class="auth_mail" title="E-mail the corresponding author} ; Sergey Trofimov ; Mikhail Ovchinnikov

关键词：Recovery strategy ; Station-keeping ; Circular restricted three-body problem ; Libration point ; Halo orbit

刊名：Advances in Space Research

出版年：2016

10.Precise halo orbit design and optimal transfer to halo orbits from earth using differential evolution

作者：Pranav Nath¹ ; ^{maywerick@gmail.com" class="auth_mail" title="E-mail the corresponding author} ; R.V. Ramanan² ; ^{rvramanan@iist.ac.in" class="auth_mail" title="E-mail the corresponding author}

关键词：Lagrangian point ; Halo orbit design ; Optimal transfer ; Restricted three body problem ; Differential correction ; Differential evolution

刊名：Advances in Space Research

出版年：2016

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