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Torques And Attitude Sensing In Earth Satellites


Torques And Attitude Sensing In Earth Satellites
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Torques And Attitude Sensing In Earth Satellites


Torques And Attitude Sensing In Earth Satellites
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Author : S. Fred Singer
language : en
Publisher: Elsevier
Release Date : 2012-12-02

Torques And Attitude Sensing In Earth Satellites written by S. Fred Singer and has been published by Elsevier this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-12-02 with Technology & Engineering categories.


Applied Mathematics and Mechanics, Volume 7: Torques and Attitude Sensing in Earth Satellites focuses on the possible torques that can affect the angular momentum of an Earth satellite. This book provides an understanding of the environment in which a satellite operates. Organized into 16 chapters, this volume starts with an overview of the application of force-free motion to space programs. This text then discusses the torque effects of a gravitational field, particularly with its gradient. Other chapters consider a particular method of gravity-gradient stabilization that utilizes a passive device to damp librations and thereby attain a vertical orientation. This book discusses as well the effects of the geomagnetic field on the angular motion of a satellite. The reader is also introduced to the method of magnetic attitude control employed in the Tiros satellite. The final chapter deals with the problem of horizon sensing, which is important for satellites requiring Earth stabilization. Astrophysicists will find this book useful.



Torques And Attitude Sensing In Earth Satellites


Torques And Attitude Sensing In Earth Satellites
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Author : Siegfried Fred Singer
language : en
Publisher:
Release Date : 1964

Torques And Attitude Sensing In Earth Satellites written by Siegfried Fred Singer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Artificial satellites categories.




Torques And Attitude Sensing In Earth Satellites


Torques And Attitude Sensing In Earth Satellites
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Author : S. Fred Singer (Siegfried Fred.)
language : en
Publisher:
Release Date : 1964

Torques And Attitude Sensing In Earth Satellites written by S. Fred Singer (Siegfried Fred.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.




Torques And Attitude Sensing In Earth Satellites Edited By S Fred Singer With Illustrations


Torques And Attitude Sensing In Earth Satellites Edited By S Fred Singer With Illustrations
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Author : Siegfried Fred SINGER
language : en
Publisher:
Release Date : 1964

Torques And Attitude Sensing In Earth Satellites Edited By S Fred Singer With Illustrations written by Siegfried Fred SINGER and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.




Satellite Attitude Control Utilizing The Earth S Magnetic Field


Satellite Attitude Control Utilizing The Earth S Magnetic Field
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Author : John S. White (writer on artificial satellites.)
language : en
Publisher:
Release Date : 1961

Satellite Attitude Control Utilizing The Earth S Magnetic Field written by John S. White (writer on artificial satellites.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Artificial satellites categories.


The torque developed by the interaction of current-carrying coils with the earth's magnetic field can be used as a means of attitude control. The degree to which the attitude of a vehicle can be maintained utilizing this torque depends on the fluctuations of the magnetic field at the satellite as the satellite orbits about the earth. Due to the nature of the torque developed only two vehicle axes can be c ntinuously controlled simultaneously. With the principle described, either a two- or three-coil system can be used to control vehicle attitude about two axes. Intermittent control about three axes can be obtained. (Author).



Attitude Control Subsystem For The Advanced Communications Technology Satellite


Attitude Control Subsystem For The Advanced Communications Technology Satellite
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Author : Alan W. Hewston
language : en
Publisher:
Release Date : 1996

Attitude Control Subsystem For The Advanced Communications Technology Satellite written by Alan W. Hewston and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Artificial satellites in telecommunication categories.




A Method For Controlling The Attitude Of A Satellite Using The Earth S Magnetic Field


A Method For Controlling The Attitude Of A Satellite Using The Earth S Magnetic Field
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Author : Wilfred Joseph Minkus
language : en
Publisher:
Release Date : 1964

A Method For Controlling The Attitude Of A Satellite Using The Earth S Magnetic Field written by Wilfred Joseph Minkus and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.


The report investigates a means of controlling the attitude of a satellite in a circular orbit about the earth by the torque due to the interaction between the earth's magnetic field and the magnetic moments produced by currents in three orthogonal coils aboard the satellite. This system has the advantage over more conventional ones in that no mass is expended in the control process. It is designed to rotate the satellite about its longitudinal axis in a minimum amount of time while limiting the deviation of this axis from the local normal to the earth. The analysis is limited to the period during which the satellite's attitude is being changed by magnetically produced torques. When these torques are not applied, gravity gradient effects act as a restoring force to align the longitudinal axis with the local normal to the earth. The method is applicable to a satellite with symmetry such that the moment of inertia about its longitudinal axis is much smaller than those about body-fixed axes lying in a plane perpendicular to it and whose moments of inertia about axes in this plane are approximately equal. The model of the earth's magnetic field that is used is a dipole with its poles located at the observed geographical positions. The control system is developed to be applicable to the general type of satellite indicated above and to all orbits except those passing close to the magnetic poles. It is then applied to a particular satellite and type of orbit of interest to RADC. (Author).



Attitude Determination For Tiros Satellites


Attitude Determination For Tiros Satellites
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Author : Joseph W. Siry
language : en
Publisher:
Release Date : 1964

Attitude Determination For Tiros Satellites written by Joseph W. Siry and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Meteorological satellites categories.




Some Notes On Attitude Control Of Earth Satellite Vehicles


Some Notes On Attitude Control Of Earth Satellite Vehicles
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Author : Warren Gillespie
language : en
Publisher:
Release Date : 1959

Some Notes On Attitude Control Of Earth Satellite Vehicles written by Warren Gillespie and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.




Fundamentals Of Spacecraft Attitude Determination And Control


Fundamentals Of Spacecraft Attitude Determination And Control
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Author : F. Landis Markley
language : en
Publisher: Springer
Release Date : 2014-05-31

Fundamentals Of Spacecraft Attitude Determination And Control written by F. Landis Markley and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-05-31 with Technology & Engineering categories.


This book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice and also provides prototype algorithms that are readily available on the author’s website. Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion. This title also provides a thorough treatise of attitude dynamics including Jacobian elliptical functions. It is the first known book to provide detailed derivations and explanations of state attitude determination and gives readers real-world examples from actual working spacecraft missions. The subject matter is chosen to fill the void of existing textbooks and treatises, especially in state and dynamics attitude determination. MATLAB code of all examples will be provided through an external website.