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[null,"1.","Record Nr.",null,"UNINA9911019181203321"]
[null,null,"Autore",null,"Tewari Ashish"]
[null,null,"Titolo",null,"Foundations of Space Dynamics"]
[null,null,"Pubbl/distr/stampa",null,"Newark : , : John Wiley & Sons, Incorporated, , 2020"]
[{"$nulls":4},"©2020"]
[null,null,"ISBN",null,"1-119-45532-4"]
[{"$nulls":4},"1-119-45533-2"]
[{"$nulls":4},"1-119-45530-8"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (371 pages)"]
[null,null,"Collana",null,"Aerospace Ser."]
[null,null,"Disciplina",null,"629.4/11"]
[null,null,"Soggetti",null,"Orbital mechanics"]
[{"$nulls":4},"Space vehicles - Dynamics"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,"Nota di contenuto",null,"Cover -- Title Page -- Copyright -- Contents -- Preface -- Chapter 1 Introduction --   1.1 Space Flight --     1.1.1 Atmosphere as Perturbing Environment --     1.1.2 Gravity as the Governing Force --     1.1.3 Topics in Space Dynamics --   1.2 Reference Frames and Time Scales --     1.2.1 Sidereal Frame --     1.2.2 Celestial Frame --     1.2.3 Synodic Frame --     1.2.4 Julian Date --   1.3 Classification of Space Missions --   1.3 Exercises --   1.3 References -- Chapter 2 Dynamics --   2.1 Notation and Basics --   2.2 Plane Kinematics --   2.3 Newton's Laws --   2.4 Particle Dynamics --   2.5 The n‐Body Problem --   2.6 Dynamics of a Body --   2.7 Gravity Field of a Body --     2.7.1 Legendre Polynomials --     2.7.2 Spherical Coordinates --     2.7.3 Axisymmetric Body --     2.7.4 Spherical Body with Radially Symmetric Mass Distribution"]
[null,null,null,"Sommario/riassunto","\"Space dynamics is one of the most important topics in aerospace engineering. It governs the satellites launched into an Earth orbit as well as lunar and interplanetary space exploration missions. The successful launching and operation of all spacecraft requires a good knowledge of space dynamics. Space dynamics can be divided into two broad categories: (i) orbital mechanics, and (ii) attitude dynamics. Orbital mechanics is a study of the translational motion of a spacecraft under the gravitational influence of either one or several large bodies. Attitude dynamics is the study of rotational motion of a rigid spacecraft about its own centre of mass, and includes both kinematical and kinetic "]
[{"$nulls":4},"description in terms of Euler angles, quaternion, or Rodrigues/modified Rodrigues parameters, and the angular velocity components.\"--"]