Download or read book Attitude Stability of a Spinning Passive Orbiting Satellite written by Leonard Meirovitch and published by . This book was released on 1967 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stability of a Spinning Passive Orbiete Satellite written by Leonard Meirovitch and published by . This book was released on 1967 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stability of a Spinning Passive Orbiting Satellite written by L. Meirovitch and published by . This book was released on 1967 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stability of Orbiting Dual Spin Satellites written by Eddy Walton White and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stability of a Class of Partially Flexible Spinning Satellites written by Thomas W. Flatley and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book ASME 65 APMW 27 written by T. R. Kane and published by . This book was released on 1965 with total page 4 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Spacecraft Dynamics and Control written by Marcel J. Sidi and published by Cambridge University Press. This book was released on 2000-07-03 with total page 434 pages. Available in PDF, EPUB and Kindle. Book excerpt: Satellites are used increasingly in telecommunications, scientific research, surveillance, and meteorology, and these satellites rely heavily on the effectiveness of complex onboard control systems. This 1997 book explains the basic theory of spacecraft dynamics and control and the practical aspects of controlling a satellite. The emphasis throughout is on analyzing and solving real-world engineering problems. For example, the author discusses orbital and rotational dynamics of spacecraft under a variety of environmental conditions, along with the realistic constraints imposed by available hardware. Among the topics covered are orbital dynamics, attitude dynamics, gravity gradient stabilization, single and dual spin stabilization, attitude maneuvers, attitude stabilization, and structural dynamics and liquid sloshing.

Download or read book Spacecraft Attitude Determination and Control written by J.R. Wertz and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 877 pages. Available in PDF, EPUB and Kindle. Book excerpt: Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. During this time, it has been difficult to obtain reference material that provided a comprehensive overview of attitude support activities. This lack of reference material has made it difficult for those not intimately involved in attitude functions to become acquainted with the ideas and activities which are essential to understanding the various aspects of spacecraft attitude support. As a result, I felt the need for a document which could be used by a variety of persons to obtain an understanding of the work which has been done in support of spacecraft attitude objectives. It is believed that this book, prepared by the Computer Sciences Corporation under the able direction of Dr. James Wertz, provides this type of reference. This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics; an introductory textbook for stu dents and professionals starting in this field; an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation and how it is determined, but who have neither the time nor the resources to pursue the varied literature on this subject; and a tool for encouraging those who could expand this discipline to do so, because much remains to be done to satisfy future needs.

Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1967 with total page 2300 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stabilization for CubeSat written by Mohammed Chessab Mahdi and published by Cambridge Scholars Publishing. This book was released on 2018-11-14 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book explores CubeSat technology, and develops a nonlinear mathematical model of a spacecraft with the assumption that the satellite is a rigid body. It places emphasis on the CubeSat subsystem, orbit dynamics and perturbations, the satellite attitude dynamic and modeling, and components of attitude determination and the control subsystem. The book focuses on the attitude stabilization methods of spacecraft, and presents gravity gradient stabilization, aerodynamic stabilization, and permanent magnets stabilization as passive stabilization methods, and spin stabilization and three axis stabilization as active stabilization methods. It also discusses the need to develop a control system design, and describes the design of three controller configurations, namely the Proportional–Integral–Derivative Controller (PID), the Linear Quadratic Regulator (LQR), and the Fuzzy Logic Controller (FLC) and how they can be used to design the attitude control of CubeSat three-axis stabilization. Furthermore, it presents the design of a suitable attitude stabilization system by combining gravity gradient stabilization with magnetic torquing, and the design of magnetic coils which can be added in order to improve the accuracy of attitude stabilization. The book then investigates, simulates, and compares possible controller configurations that can be used to control the currents of magnetic coils when magnetic coils behave as the actuator of the system.

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stabilization of Satellites in Orbit written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Guidance and Control Panel and published by . This book was released on 1971 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Large Attitude Motions and Stability Due to Gravity of a Satellite with Passive Damping in an Orbit of Arbitrary Eccentricity about an Oblate Body written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1962 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Attitude Stability of an Orbiting Satellite Containing Flexible Antennas and Spinning Rotors written by Phillip Eugene Sanders and published by . This book was released on 1976 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study considers the attitude stability of a gyrostat satellite containing flexible antennas, in which any, or all, of the rotors or antennas may be misaligned with the main body principal axes. The problem is formulated in general for any number of rigid, symmetrical, spinning rotors which are fixed relative to the body and for any number of antennas, modeled as rigid rods connected by torsional springs. The stability analysis is based on the Liapunov direct method, using the Hamiltonian as the Liapunov function. Examples are presented for a gravity-stabilized satellite containing one constant-speed rotor and two antennas of two rods each. The antenna misalignment and motion is restricted to the xz-plane. Results show that for a rotor misalignment, the largest deviation from the position defined by the body principal axes aligning with the orbital axes occurs when the misalignment is toward the orbit tangent. Misalignment of the antennas has no effect on the body equilibrium position except when the rotor was also misaligned. In that case, the body equilibrium angles were reduced. (Author).

Download or read book Attitude Stabilization of Satellites in Orbit written by ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (France) and published by . This book was released on 1971 with total page 155 pages. Available in PDF, EPUB and Kindle. Book excerpt: ;Contents: Rotational dynamics; Spacecraft attitude sensors with emphasis on the orbiting astronomical observatory; Passive and semi-active attitude stabilizations - dual spin satellites; Passive and semi-active attitude stabilizations - flexible spacecraft; Active stabilization; Esro td satellite pneumatic system; Sirio attitude measurement and control system; Apollo spacecraft.

Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1968 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt: