Satellite Attitude Control Utilizing The Earths Magnetic Field

Author : John S. White (writer on artificial satellites.)
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.55/5 ( download)

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Download or read book Satellite Attitude Control Utilizing the Earth's Magnetic Field written by John S. White (writer on artificial satellites.) and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).

Author : R. E. TOEPFER
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.58/5 ( download)

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Download or read book Satellite Attitude Control Using the Earth's Magnetic Field written by R. E. TOEPFER and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Wilfred Joseph Minkus
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.36/5 ( download)

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Download or read book A Method for Controlling the Attitude of a Satellite Using the Earth's Magnetic Field written by Wilfred Joseph Minkus and published by . This book was released on 1964 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).

Author : Karthik G. Ganesh
Publisher :
ISBN 13 :
Total Pages : 125 pages
Book Rating : 4.31/5 ( download)

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Download or read book Controls Algorithm for a Satellite Using Earth's Magnetic Field written by Karthik G. Ganesh and published by . This book was released on 2007 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document describes the design, analysis of Orbit Maneuvers and Attitude Control for NanoSat class satellites, which uses an electro-magnetic force controller which was proposed by the Florida Space Institute (FSI).

Author : THOMAS TERRELL MCELROY
Publisher :
ISBN 13 :
Total Pages : 225 pages
Book Rating : 4.84/5 ( download)

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Download or read book ATTITUDE DETERMINATION AND CONTROL OF A SPINNING SATELLITE USING THE EARTH'S MAGNETIC FIELD.. written by THOMAS TERRELL MCELROY and published by . This book was released on 1973 with total page 225 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : V. Matthewson
Publisher :
ISBN 13 :
Total Pages : 41 pages
Book Rating : 4.46/5 ( download)

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Download or read book Attitude Control Using the Earth's Magnetic Field written by V. Matthewson and published by . This book was released on 2000 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Warren Gillespie
Publisher :
ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.57/5 ( download)

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Download or read book Some Notes on Attitude Control of Earth Satellite Vehicles written by Warren Gillespie and published by . This book was released on 1959 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : James J. Adams
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.93/5 ( download)

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Download or read book Simulator Study of a Satellite Attitude Control System Using Inertia Wheels and a Magnet written by James J. Adams and published by . This book was released on 1963 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.27/5 ( download)

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Download or read book Observations of the Earth's Magnetic Field from the Shuttle written by and published by . This book was released on 1986 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Nitin Seth
Publisher :
ISBN 13 : 9780494600139
Total Pages : 82 pages
Book Rating : 4.36/5 ( download)

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Download or read book Hybrid Magnetic Attitude Controller for Low Earth Orbit Satellites Using the Time-varying Linear Quadratic Regulator written by Nitin Seth and published by . This book was released on 2009 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt: The following is a study of an attitude control system (ACS) for a low earth orbit nanosatellite. Control actuation is applied using three reaction wheels and three mutually orthogonal current-driven magnetorquers which produce torques by interacting with the earth's magnetic field. Control torques are distributed amongst the actuators allowing them to work together in concert. This type of control is referred to as hybrid magnetic attitude control. To account for the nearly periodic behavior of the earth's magnetic field, control torques are assigned using periodic and optimal control theory. The primary focus is to apply the time-varying Linear Quadratic Regulator controller to test the stability and energy consumption of the ACS when reaction wheels are removed from the control law, or are simulated to be missing. Other situations studied include the effects of control saturation, introducing uncertainty in the orbital inclination, and observing performance as the number of magnetic coils is increased.