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Modeling And Parameter Estimation Of Spacecraft Lateral Fuel Slosh
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Book Synopsis Modeling and Parameter Estimation of Spacecraft Lateral Fuel Slosh by : Yadira Rodriguez Chatman
Download or read book Modeling and Parameter Estimation of Spacecraft Lateral Fuel Slosh written by Yadira Rodriguez Chatman and published by . This book was released on 2008 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt: "This research focuses on the parameter estimation of a SimMechanics model of the simulated spacecraft propellant tank with diaphragms using lateral fuel slosh experiment data."--Leaf iv.
Book Synopsis Parameter Estimation of Spacecraft Fuel Slosh Using Pendulum Analogs by : Keith L. Schlee
Download or read book Parameter Estimation of Spacecraft Fuel Slosh Using Pendulum Analogs written by Keith L. Schlee and published by . This book was released on 2006 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt: "This research is a pioneering effort toward automating the parameter identification process by using a MATLAB/SimMechanics based computer simulation modeling of a free-surface fuel slosh in a spherical propellant tank of a spacecraft."--Leaf iv.
Book Synopsis Study of Modeling and Adaptive Control of Spacecraft with Fuel Slosh by : Hesham M. Shageer
Download or read book Study of Modeling and Adaptive Control of Spacecraft with Fuel Slosh written by Hesham M. Shageer and published by . This book was released on 2006 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Investigation of the Fluid Behavior and Damping Parameters of Diaphragm-implemented Spacecraft Propellant Tanks by : Brian Andrew Lenahen
Download or read book An Investigation of the Fluid Behavior and Damping Parameters of Diaphragm-implemented Spacecraft Propellant Tanks written by Brian Andrew Lenahen and published by . This book was released on 2012 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Current research is directed at computationally modeling various fuel slosh scenarios which a spacecraft could potentially experience while in orbit. Simulations to be tested include, but are not limited to, different diaphragm materials within the tank, various diaphragm shapes within the tank and testing at the system's natural frequency. Upon acquiring sufficient and acceptable results from computational tests, similar models are created for experimental testing in the Embry-Riddle Aeronautical University Fuel Slosh Test Facility."--Leaf iv.
Book Synopsis Dynamic Stability of Space Vehicles: Testing for booster propellant sloshign parameters, by D. M. Eggleston by : General Dynamics Corporation
Download or read book Dynamic Stability of Space Vehicles: Testing for booster propellant sloshign parameters, by D. M. Eggleston written by General Dynamics Corporation and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Advances in Spacecraft Technologies by : Jason Hall
Download or read book Advances in Spacecraft Technologies written by Jason Hall and published by IntechOpen. This book was released on 2011-02-14 with total page 610 pages. Available in PDF, EPUB and Kindle. Book excerpt: The development and launch of the first artificial satellite Sputnik more than five decades ago propelled both the scientific and engineering communities to new heights as they worked together to develop novel solutions to the challenges of spacecraft system design. This symbiotic relationship has brought significant technological advances that have enabled the design of systems that can withstand the rigors of space while providing valuable space-based services. With its 26 chapters divided into three sections, this book brings together critical contributions from renowned international researchers to provide an outstanding survey of recent advances in spacecraft technologies. The first section includes nine chapters that focus on innovative hardware technologies while the next section is comprised of seven chapters that center on cutting-edge state estimation techniques. The final section contains eleven chapters that present a series of novel control methods for spacecraft orbit and attitude control.
Book Synopsis Liquid Sloshing Dynamics by : Raouf A. Ibrahim
Download or read book Liquid Sloshing Dynamics written by Raouf A. Ibrahim and published by . This book was released on 2005-09 with total page 972 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book deals with almost every aspect of liquid sloshing dynamics.
Book Synopsis Modelling and Control of Space Vehicles with Fuel Slosh Dynamics by : Mahmut Reyhanoglu
Download or read book Modelling and Control of Space Vehicles with Fuel Slosh Dynamics written by Mahmut Reyhanoglu and published by . This book was released on 2011 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Modelling and Control of Space Vehicles with Fuel Slosh Dynamics.
Book Synopsis Geometric Reduced Hybrid System and Parametric Worst Case Analysis for a Science Satellite by : Shan Tang
Download or read book Geometric Reduced Hybrid System and Parametric Worst Case Analysis for a Science Satellite written by Shan Tang and published by . This book was released on 2008 with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stochastic Models: Estimation and Control: v. 2 by : Maybeck
Download or read book Stochastic Models: Estimation and Control: v. 2 written by Maybeck and published by Academic Press. This book was released on 1982-08-10 with total page 307 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stochastic Models: Estimation and Control: v. 2
Book Synopsis Fundamentals of Spacecraft Attitude Determination and Control by : F. Landis Markley
Download or read book Fundamentals of Spacecraft Attitude Determination and Control written by F. Landis Markley and published by Springer. This book was released on 2014-05-31 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Spacecraft Attitude Determination and Control by : J.R. Wertz
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.
Book Synopsis Fundamentals of Rocket Propulsion by : DP Mishra
Download or read book Fundamentals of Rocket Propulsion written by DP Mishra and published by CRC Press. This book was released on 2017-07-20 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.
Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout
Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Book Synopsis Theory of the Fluid Oscillations in a Circular Cylindrical Ring Tank Partially Filled with Liquid by : Helmut F. Bauer
Download or read book Theory of the Fluid Oscillations in a Circular Cylindrical Ring Tank Partially Filled with Liquid written by Helmut F. Bauer and published by . This book was released on 1960 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Liquid Rocket Valve Components by : H. J. Ellis
Download or read book Liquid Rocket Valve Components written by H. J. Ellis and published by . This book was released on 1973 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Space Vehicle Dynamics and Control by : Bong Wie
Download or read book Space Vehicle Dynamics and Control written by Bong Wie and published by AIAA. This book was released on 1998 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: A textbook that incorporates the latest methods used for the analysis of spacecraft orbital, attitude, and structural dynamics and control. Spacecraft dynamics is treated as a dynamic system with emphasis on practical applications, typical examples of which are the analysis and redesign of the pointing control system of the Hubble Space Telescope and the analysis of an active vibrations control for the COFS (Control of Flexible Structures) Mast Flight System. In addition to the three subjects mentioned above, dynamic systems modeling, analysis, and control are also discussed. Annotation copyrighted by Book News, Inc., Portland, OR
