03922nam 2200661Ia 450 991045318460332120200520144314.01-281-95629-59786611956295981-281-063-3(CKB)1000000000538102(EBL)1679699(OCoLC)879023942(SSID)ssj0000142028(PQKBManifestationID)11134545(PQKBTitleCode)TC0000142028(PQKBWorkID)10090353(PQKB)11255822(MiAaPQ)EBC1679699(WSP)00004402(Au-PeEL)EBL1679699(CaPaEBR)ebr10255707(EXLCZ)99100000000053810220000629d2001 uy 0engurcn|||||||||txtccrDynamics and mission design near libration pointsVol. IFundamentals : the case of collinear libration points[electronic resource]Singapore ;River Edge, N.J. World Scientific20011 online resource (462 p.)World scientific monograph series in mathematics ;vol. 2Description based upon print version of record.981-02-4285-9 Includes bibliographical references.Contents; Foreword; Preface: Introduction: Libration Points and Station Keeping; 0.1 The Neighborhood of Libration Points as a Useful Place for Spacecrafts; 0.1.1 The Libration Points in the Restricted Three-body Problem0.1.2 The Libration Points in Perturbations of the Restricted Threebody Problem 0.1.3 Possible Missions Around the Libration Points.1.4 The Real Nominal Quasi-periodic Orbit; 0.2 Station Keeping of Libration Point Orbits; 0.2.1 Unstable Nominal Orbits0.2.2 Requirements for an On/off Control Chapter 1 Bibliographical Survey; 1.1 Numerical Results for Three-dimensional Periodic Orbits Around L1, L2 and L3; 1.1.1 References; 1.1.2 Equations. General Properties; 1.1.3 Linear Theory Around the Equilibrium Points; 1.1.4 Description of the Results1.2 Analytic Results for Halo Orbits Associated to L1, L2 and L3 1.2.1 References; 1.2.2 Equations of Motion; 1.2.3 Construction of Halo Periodic Solutions; 1.3 Motion Near L4 and L5; 1.3.1 References; 1.3.2 The Triangular Equilibrium Points, Location and Stability; 1.3.3 Numerical Explorations; 1.3.4 Analytic Results; 1.4 Station Keeping1.4.1 References 1.4.2 The Control of Libration Point Satellites; 1.4.3 Station Keeping for a Translunar Station; 1.4.4 Control of an Unstable Periodic Orbit; 1.4.5 Station Keeping for the ISEE-C. Algorithm and Results ; 1.4.6 Additional WorkChapter 2 Halo Orbits. Analytic and Numerical StudyIn this book the problem of station keeping is studied for orbits near libration points in the solar system. The main focus is on orbits near halo ones in the (Earth+Moon)-Sun system. Taking as starting point the restricted three-body problem, the motion in the full solar system is considered as a perturbation of this simplified model. All the study is done with enough generality to allow easy application to other primary-secondary systems as a simple extension of the analytical and numerical computations. Contents: Bibliographical Survey Halo Orbits. Analytical andWorld Scientific monograph series in mathematics ;v. 2.Three-body problemLagrangian pointsElectronic books.Three-body problem.Lagrangian points.521.3Gómez G(Gerard)878196MiAaPQMiAaPQMiAaPQBOOK9910453184603321Dynamics and mission design near libration points1960521UNINA