Volume 30, Issue 3 No AccessRelative Spacecraft Motion in a Central Force FieldDaniel Condurache and Vladimir MartinuşiDaniel Condurache Technical University “Gheorghe Asachi”, 700050 Iaşi, RomaniaSearch for more papers by this author and Vladimir Martinuşi Technical University “Gheorghe Asachi”, 700050 Iaşi, RomaniaSearch for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/1.26361SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited bySatellites’ orbits in the Sun–Earth–Moon system16 May 2023 | Celestial Mechanics and Dynamical Astronomy, Vol. 135, No. 3A Full-Body Relative Orbital Motion of Spacecraft Using Dual Tensor Algebra and Dual Quaternions11 March 2023 | Mathematics, Vol. 11, No. 6Forced Keplerian orbits in the Earth–Moon system1 Apr 2022 | Acta Astronautica, Vol. 193Exact Closed-Form Solutions of the Motion in Non-Inertial Reference Frames, Using the Properties of Lie Groups SO3 and SE318 October 2021 | Symmetry, Vol. 13, No. 10On Six DOF Relative Orbital Motion of Satellites20 June 2018On six DOF relative orbital motion of spacecrafts. A complete onboard solution1 November 2017 | Journal of Engineering Sciences and Innovation, Vol. 2, No. 4The theory of asynchronous relative motion I: time transformations and nonlinear corrections21 September 2016 | Celestial Mechanics and Dynamical Astronomy, Vol. 127, No. 3Onboard Exact Solution to the Full-Body Relative Orbital Motion ProblemD. Condurache and A. Burlacu26 August 2016 | Journal of Guidance, Control, and Dynamics, Vol. 39, No. 12Second Order Theory for Relative Orbital ElementsBrett A. Newman9 September 2016Prox-1 University-Class Mission to Demonstrate Automated Proximity OperationsDavid A. Spencer, Sean B. Chait, Peter Z. Schulte, Kevin J. Okseniuk and Michael Veto28 July 2016 | Journal of Spacecraft and Rockets, Vol. 53, No. 5A Short Vector Solution of the Foucault Pendulum Problem1 Jan 2015 | World Journal of Mechanics, Vol. 05, No. 02Relative Orbital Elements Formulation Based upon the Clohessy-Wiltshire Equations10 February 2015 | The Journal of the Astronautical Sciences, Vol. 61, No. 4On Board Exact Solution to the Full Body Relative Orbital Motion ProblemDaniel Condurache and Adrian Burlacu1 August 2014Solutions and periodicity of satellite relative motion under even zonal harmonics perturbations13 September 2011 | Celestial Mechanics and Dynamical Astronomy, Vol. 111, No. 4Optimal Satellite Formation Establishment about an Oblate PlanetVladimir Martinusi and Pini Gurfil14 June 2012State Space Analysis for The Relative Spacecraft Motion in Geopotential FieldsDaniel Condurache and Vladimir Martinusi14 June 2012Quaternionic Exact Solution to the Relative Orbital Motion Problem Daniel Condurache and Vladimir Martinusi 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 33, No. 4The Modeling and Simulation of Rendezvous and Docking1 Jan 2010Analytic Solution to the Relative Orbital Motion Around an Oblate PlanetDaniel Condurache and Vladimir Martinusi14 June 2012Exact solution to the relative orbital motion in eccentric orbits10 February 2009 | Solar System Research, Vol. 43, No. 1Exact Solution to the Relative Orbital Motion in a Central Force Field1 Dec 2008Foucault Pendulum-like problems: A tensorial approach1 Oct 2008 | International Journal of Non-Linear Mechanics, Vol. 43, No. 8 What's Popular Volume 30, Number 3May 2007 Metrics Crossmark TopicsAstronomyCelestial Coordinate SystemCelestial MechanicsGuidance, Navigation, and Control SystemsPlanetary Science and ExplorationPlanetsSpace MissionsSpace Science and TechnologySpacecraft GuidanceSpacecraft Guidance and Control KeywordsSpacecraft MotionSpecific Angular MomentumSatellitesOrbital ElementsSpacecraft DynamicsRight AscensionSpace MissionsEarthDigital Published online23 May 2012