Constant-Thrust Orbit-Raising Transfer Charts

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ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Constant-Thrust Orbit-Raising Transfer Charts by :

Download or read book Constant-Thrust Orbit-Raising Transfer Charts written by and published by . This book was released on 1993 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report outlines a method to generate minimum-fuel trajectories between coplanar circular orbits for a vehicle with constant thrust. The rocket equation models the effects of continuous fuel expenditure while also serving to recast the solution in terms of accumulated velocity change. These orbit-raising solutions are globally mapped with no restrictions on initial thrust magnitude, intermediate eccentricity, or number of revolutions of the central body. Several examples are presented to verify the transfer charts and familiarize the reader with their use. These charts are useful tools for mission planners and satellite designers to assess preliminary fuel requirements for constant-thrust systems or to compare different propulsion technologies ... Electric Propulsion, Thrust, Thruster, Efficiency, Orbits, Flight Maneuvers, Trajectories, Satellites (Artificial).

Trajectories with Constant Tangential Thrust in Central Gravitational Fields

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ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Trajectories with Constant Tangential Thrust in Central Gravitational Fields by : W. E. Moeckel

Download or read book Trajectories with Constant Tangential Thrust in Central Gravitational Fields written by W. E. Moeckel and published by . This book was released on 1960 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 538 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Optimal Continuous-Thrust Orbit Transfers

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ISBN 13 : 9781423585305
Total Pages : 103 pages
Book Rating : 4.5/5 (853 download)

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Book Synopsis Optimal Continuous-Thrust Orbit Transfers by : James Dana Thorne

Download or read book Optimal Continuous-Thrust Orbit Transfers written by James Dana Thorne and published by . This book was released on 1996-06-01 with total page 103 pages. Available in PDF, EPUB and Kindle. Book excerpt: The minimum time orbital transfer problem for spacecraft with steerable, continuous thrust of constant magnitude may be solved using Euler- Lagrange theory, which leads to the optimal control law in terms of Lagrange multipliers. However, the initial values of the Lagrange multipliers are not known from the orbital boundary conditions. Using analytical and empirical results, the optimal initial costates are modeled as functions of the problem parameters which are the initial thrust acceleration, A, and the final orbit radius, H, in canonical units. For circle to circle, coplanar orbit transfers, these approximate initial costate models lead to convergence in the shooting method for all practical values of A and H. The models also lead to convergence for a wide rang of other problems, including circle to hyperbola transfers and non-coplanar transfers. To counter the extreme sensitivity to small changes in the initial costate conditions, a dynamic step limiter is introduced which improve the convergence properties.

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 814 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1968 with total page 814 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Nonsingular Astrodynamics

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Publisher : Cambridge University Press
ISBN 13 : 1108472362
Total Pages : 481 pages
Book Rating : 4.1/5 (84 download)

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Book Synopsis Applied Nonsingular Astrodynamics by : Jean Albert Kéchichian

Download or read book Applied Nonsingular Astrodynamics written by Jean Albert Kéchichian and published by Cambridge University Press. This book was released on 2018-08-16 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: This essential book is the first comprehensive exposition in the area of optimal low-thrust orbit transfer using non-singular variables.

Analytical Equations for Orbital Transfer Maneuvers of a Vehicle Using Constant Low Thrust

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (132 download)

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Book Synopsis Analytical Equations for Orbital Transfer Maneuvers of a Vehicle Using Constant Low Thrust by : Samuel J. Domino (2LT, USAF., Jr)

Download or read book Analytical Equations for Orbital Transfer Maneuvers of a Vehicle Using Constant Low Thrust written by Samuel J. Domino (2LT, USAF., Jr) and published by . This book was released on 1981 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Spaceflight Mechanics 2000

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Publisher : Univelt
ISBN 13 :
Total Pages : 928 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Spaceflight Mechanics 2000 by : Kyle T. Alfriend

Download or read book Spaceflight Mechanics 2000 written by Kyle T. Alfriend and published by Univelt. This book was released on 1994 with total page 928 pages. Available in PDF, EPUB and Kindle. Book excerpt: Published for the American Astronautical Society (AAS). The August 1993 conference was hosted by the AAS and co-sponsored by the American Institute of Aeronautics and Astronautics. The proceedings cover topics including attitude determination and control, TOPEX orbit determination and control, orbit determination, orbit transfer, tethers, mission analysis (planetary/Earth/general/trajectories), navigation, rendezvous, attitude dynamics and control, flexible body dynamics and control, and orbit dynamics. Additional papers from the conference are available on a microfiche supplement (v.70, AAS Microfiche Series); these are represented in the present volumes by an abstract with reference to the supplement. No subject index. Annotation copyright by Book News, Inc., Portland, OR

Fundamentals of Astrodynamics and Applications

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Publisher : Springer Science & Business Media
ISBN 13 : 9780792369035
Total Pages : 1002 pages
Book Rating : 4.3/5 (69 download)

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Book Synopsis Fundamentals of Astrodynamics and Applications by : D.A. Vallado

Download or read book Fundamentals of Astrodynamics and Applications written by D.A. Vallado and published by Springer Science & Business Media. This book was released on 2001-06-30 with total page 1002 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fundamentals of Astrodynamics and Applications is rapidly becoming the standard astrodynamics reference for those involved in the business of spaceflight. What sets this book apart is that nearly all of the theoretical mathematics is followed by discussions of practical applications implemented in tested software routines. For example, the book includes a compendium of algorithms that allow students and professionals to determine orbits with high precision using a PC. Without a doubt, when an astrodynamics problem arises in the future, it will become standard practice for engineers to keep this volume close at hand and `look it up in Vallado'. While the first edition was an exceptionally useful and popular book throughout the community, there are a number of reasons why the second edition will be even more so. There are many reworked examples and derivations. Newly introduced topics include ground illumination calculations, Moon rise and set, and a listing of relevant Internet sites. There is an improved and expanded discussion of coordinate systems, orbit determination, and differential correction. Perhaps most important is that all of the software routines described in the book are now available for free in FORTRAN, PASCAL, and C. This makes the second edition an even more valuable text and superb reference.

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 1576 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Government Reports Announcements & Index by :

Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1993-12 with total page 1576 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Optimal Continuous-thrust Orbit Transfers

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Publisher :
ISBN 13 :
Total Pages : 101 pages
Book Rating : 4.:/5 (348 download)

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Book Synopsis Optimal Continuous-thrust Orbit Transfers by : Jim Thorne

Download or read book Optimal Continuous-thrust Orbit Transfers written by Jim Thorne and published by . This book was released on 1996 with total page 101 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Automatic Control in Aerospace

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Publisher :
ISBN 13 :
Total Pages : 458 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Automatic Control in Aerospace by :

Download or read book Automatic Control in Aerospace written by and published by . This book was released on 1994 with total page 458 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analytical Equations for Orbital Transfer Maneuvers of a Vehicle Using Constant Low Thrust

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ISBN 13 :
Total Pages : 45 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Analytical Equations for Orbital Transfer Maneuvers of a Vehicle Using Constant Low Thrust by :

Download or read book Analytical Equations for Orbital Transfer Maneuvers of a Vehicle Using Constant Low Thrust written by and published by . This book was released on 1981 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: The object of this study is to derive a set of equations which predict the results of orbital maneuvers of vehicles using constant low thrust. These equations are developed by simplifying the problem to circular orbits in a two-body dynamic system. The results are presented in three parts. The first part solves for the equation of the coplanar radius change problem. The second finds the equation for the minimum fuel inclination change problem. The third part of this study puts the equations from the first two parts together to solve a minimum fuel transfer problem involving both radius and inclination changes. The solution of the minimum fuel transfer problem is not to perform the total radius change and then perform the total inclination change. Instead, the solution is to perform both radius and inclination changes on a per orbit basis.

The Journal of the Astronautical Sciences

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ISBN 13 :
Total Pages : 536 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis The Journal of the Astronautical Sciences by :

Download or read book The Journal of the Astronautical Sciences written by and published by . This book was released on 1994 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Astrodynamics

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ISBN 13 :
Total Pages : 944 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Astrodynamics by :

Download or read book Astrodynamics written by and published by . This book was released on 1994 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-thrust Transfer Between Circular Orbits

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ISBN 13 :
Total Pages : 418 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Low-thrust Transfer Between Circular Orbits by : Eugene Levin

Download or read book Low-thrust Transfer Between Circular Orbits written by Eugene Levin and published by . This book was released on 1958 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Nearly Circular Transfer Trajectories for Descending Satellites

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Nearly Circular Transfer Trajectories for Descending Satellites by : George M. Low

Download or read book Nearly Circular Transfer Trajectories for Descending Satellites written by George M. Low and published by . This book was released on 1959 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Simplified expressions describing the transfer from a satellite orbit to the point of atmospheric entry are derived. The expressions are limited to altitude changes that are small compared with the earth's radius, and velocity changes that are small compared with satellite velocity. They are further restricted to motion about a spherical, nonrotating earth. The transfer trajectory resulting from the application of thrust in any direction at any point in an elliptic orbit is considered. Expressions for errors in distance (miss distance) and entry angle due to an initial misalinement and magnitude error of the deflecting thrust are presented. The guidance and accuracy requirements to establish a circular orbit, and orbit corrections are also discussed.