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Author : Andrea Milani,Giovanni Gronchi
Publisher : Cambridge University Press
Page : 393 pages
File Size : 47,9 Mb
Release : 2010
Category : Mathematics
ISBN : 9780521873895
Presents new algorithms for determining orbits; ideal for graduate students and researchers in applied mathematics, physics, astronomy and aerospace engineering.
Author : Bob Schutz,Byron Tapley,George H. Born
Publisher : Elsevier
Page : 563 pages
File Size : 48,5 Mb
Release : 2004-06-26
Category : Science
ISBN : 9780080541730
Statistical Orbit Determination presents fundmentals of orbit determination--from weighted least squares approaches (Gauss) to today's high-speed computer algorithms that provide accuracy within a few centimeters. Numerous examples and problems are provided to enhance readers' understanding of the material. Covers such topics as coordinate and time systems, square root filters, process noise techniques, and the use of fictitious parameters for absorbing un-modeled and incorrectly modeled forces acting on a satellite. Examples and exercises serve to illustrate the principles throughout each chapter.
Author : Oliver Montenbruck,Eberhard Gill
Publisher : Springer Science & Business Media
Page : 371 pages
File Size : 52,6 Mb
Release : 2012-12-06
Category : Science
ISBN : 9783642583513
This modern presentation guides readers through the theory and practice of satellite orbit prediction and determination. Starting from the basic principles of orbital mechanics, it covers elaborate force models as well as precise methods of satellite tracking. The accompanying CD-ROM includes source code in C++ and relevant data files for applications. The result is a powerful and unique spaceflight dynamics library, which allows users to easily create software extensions. An extensive collection of frequently updated Internet resources is provided through WWW hyperlinks.
Author : William E. Wiesel
Publisher : CreateSpace
Page : 154 pages
File Size : 44,8 Mb
Release : 2010-06-14
Category : Science
ISBN : 1453611983
Modern Orbit Determination is an introduction to the applications of estimation theory to orbit determination. Beginning with the deterministic point of view, the author moves towards the more modern stochastic viewpoint. The fact that the degree of determinism present is an engineering decision is emphasized.
Author : Howard D Curtis
Publisher : Elsevier
Page : 744 pages
File Size : 45,9 Mb
Release : 2009-10-26
Category : Technology & Engineering
ISBN : 9780080887845
Orbital Mechanics for Engineering Students, Second Edition, provides an introduction to the basic concepts of space mechanics. These include vector kinematics in three dimensions; Newton’s laws of motion and gravitation; relative motion; the vector-based solution of the classical two-body problem; derivation of Kepler’s equations; orbits in three dimensions; preliminary orbit determination; and orbital maneuvers. The book also covers relative motion and the two-impulse rendezvous problem; interplanetary mission design using patched conics; rigid-body dynamics used to characterize the attitude of a space vehicle; satellite attitude dynamics; and the characteristics and design of multi-stage launch vehicles. Each chapter begins with an outline of key concepts and concludes with problems that are based on the material covered. This text is written for undergraduates who are studying orbital mechanics for the first time and have completed courses in physics, dynamics, and mathematics, including differential equations and applied linear algebra. Graduate students, researchers, and experienced practitioners will also find useful review materials in the book. NEW: Reorganized and improved discusions of coordinate systems, new discussion on perturbations and quarternions NEW: Increased coverage of attitude dynamics, including new Matlab algorithms and examples in chapter 10 New examples and homework problems
Author : Guochang Xu,Jia Xu
Publisher : Springer Science & Business Media
Page : 444 pages
File Size : 45,7 Mb
Release : 2013-06-12
Category : Science
ISBN : 9783642327933
The development of the orbits theory lags behind the development of satellite technology. This book provides, for the first time in the history of human satellite development, the complete third order solution of the orbits under all possible disturbances. It describes the theory of satellite orbits, derives the complete solutions of the orbital disturbances, describes the algorithms of orbits determination based on the theory, describes the applications of the theory to the phenomenon of the satellite formation physically. The subjects include: Orbits Motion Equations, Disturbance theory, Solutions of the differential Equations, Algorithms of Orbits determinations, Applications of the theory to the satellite formation.
Author : Dan L. Boulet
Publisher : Willmann-Bell
Page : 592 pages
File Size : 45,8 Mb
Release : 1991
Category : Computers
ISBN : UOM:39015024992649
Author : Guochang Xu
Publisher : Springer Science & Business Media
Page : 236 pages
File Size : 43,8 Mb
Release : 2008-08-15
Category : Science
ISBN : 9783540785224
The purpose of this reference and handbook is to describe and to derive the analytic solutionsoftheequationsofsatellitemotionperturbedbyextraterrestrialandgeo- tential disturbances of the second order. The equations of satellite motion perturbed by extraterrestrial disturbances are solved by means of discretization and appr- imated potential function as well as Gaussian equations. The equations perturbed by geopotential disturbances are solved by symbolic mathematical operations. The traditional problem of singularity in the solutions is solved by so-called singulari- free orbit theory. Simpli?ed disturbed equations of motion are proposed to simplify the solutions. Applications of the theory for analytic orbit determination are also discussed. Indeed, this is the ?rst book since the satellite era, which describes s- tematically the orbit theory with analytical solutions, with respect to all of extrat- restrial and geopotential disturbances of the second order, and the solutions are free of singularity. Based on such a theory, the algorithms of orbit determination can be renewed; deeper insight into the physics of disturbances becomes possible; the way to a variety of new applications and re?nements is opened. My primary knowledge of the orbit theory came from my education of mat- matics while studying physics and theoretical mechanics (1981). My ?rst practical experience with orbit came from the research activity at the Technical University (TU) Berlin on orbit corrections of the satellite altimetry data (1988–1992). The extensive experience on orbit came from the GPS/Galileo software development for orbit determination and geopotential mapping at the GFZ (2001–2004).
Author : Alessandro de Iaco Veris
Publisher : Springer
Page : 1309 pages
File Size : 46,8 Mb
Release : 2017-11-28
Category : Technology & Engineering
ISBN : 9783319622200
This modern textbook guides the reader through the theory and practice of the motion and attitude control of space vehicles. It first presents the fundamental principles of spaceflight mechanics and then addresses more complex concepts and applications of perturbation theory, orbit determination and refinement, space propulsion, orbital maneuvers, interplanetary trajectories, gyroscope dynamics, attitude control, and rocket performance. Many algorithms used in the modern practice of trajectory computation are also provided. The numerical treatment of the equations of motion, the related methods, and the tables needed to use them receive particular emphasis. A large collection of bibliographical references (including books, articles, and items from the "gray literature") is provided at the end of each chapter, and attention is drawn to many internet resources available to the reader. The book will be of particular value to undergraduate and graduate students in aerospace engineering.
Author : Pedro Ramon Escobal
Publisher : Unknown
Page : 479 pages
File Size : 52,9 Mb
Release : 1978
Category : Artificial satellites
ISBN : OCLC:869831247
Author : Krzysztof Sośnica
Publisher : Astronomical Institute, University of Bern, Switzerland
Page : 253 pages
File Size : 47,6 Mb
Release : 2014-04-07
Category : Science
ISBN : 9788393889808
The contribution of Satellite Laser Ranging (SLR) to the definition of the origin of the reference frame (geocenter coordinates), the global scale, and low degree coefficients of the Earth's gravity field is essential due to the remarkable orbit stability of geodetic satellites and the accuracy of laser observations at a level of a few millimeters. Considering these aspects, SLR has an exceptional potential in establishing global networks and deriving geodetic parameters of the supreme quality. SLR faces today the highest requirements of the Global Geodetic Observing System (GGOS) yielding 1 mm of long-term station coordinate and 0.1 mm/y of station velocity stability. The goal of this work is to assess the contribution of the latest models and corrections to the SLR-derived parameters, to enhance the quality and reliability of the SLR-derived products, and to propose a new approach of orbit parameterization for low orbiting geodetic satellites. The impact of orbit perturbations is studied in detail, including perturbing forces of gravitational origin (Earth's gravity field, ocean and atmosphere tides) and perturbing forces of non-gravitational origin (atmospheric drag, the Yarkovsky effect, albedo and Earth's infrared radiation pressure). A multi-satellite combined solution is obtained using SLR observations to LAGEOS-1, LAGEOS-2, Starlette, Stella, and AJISAI. The quality of the SLR-derived parameters from the combined solution is compared with external solutions. The Earth rotation parameters are compared to the IERS-08-C04 series and the GNSS-derived series, whereas the time variable Earth's gravity field coefficients are compared to the CHAMP and GRACE-derived results.
Author : Pedro Ramon Escobal
Publisher : Unknown
Page : 492 pages
File Size : 47,6 Mb
Release : 1965
Category : Science
ISBN : UCAL:B4118340
Author : John E. Prussing,Bruce A. Conway
Publisher : Oxford University Press, USA
Page : 0 pages
File Size : 44,7 Mb
Release : 2013
Category : Orbital mechanics
ISBN : 0199837708
For nearly two decades, Orbital Mechanics by John E. Prussing and Bruce A. Conway has been the most authoritative textbook on space trajectories and orbital transfers. Completely revised and updated, this edition provides: * Current data and statistics, along with coverage of new research and the most recent developments in the field * Three new chapters: "The Three-Body Problem" (Ch. 4), "Continuous-Thrust Transfer" (Ch. 8), and "Canonical Systems and the Lagrange Equations" (Ch. 12) * New material on multiple-revolution Lambert solutions, gravity-assist applications, and the state transition matrix for a general conic orbit * New examples and problems throughout * A new Companion Website with PowerPoint slides (www.oup.com/us/prussing)
Author : Victor Szebehely
Publisher : Elsevier
Page : 765 pages
File Size : 41,9 Mb
Release : 2014-09-30
Category : Science
ISBN : 9780323163392
Celestial Mechanics and Astrodynamics
Author : Victor G. Szebehely
Publisher : Unknown
Page : 198 pages
File Size : 55,6 Mb
Release : 1989
Category : Science
ISBN : UOM:39015018503311
"In this well-written textbook, one of the world's leading authorities provides an expert introduction to the principles of orbital mechanics, with applications to the dynamics of space probes, artificial satellites, and members of the solar system. In Professor Szebehely's own words, his aim is "to infatuate students with the beauty of celestial mechanics, to emphasize the basic and simple principles, and to offer as challenges the fascinating, unsolved problems in this field." "--Back cover.
