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Author : University of Michigan. Engineering Summer Conferences
Publisher : Unknown
Page : 580 pages
File Size : 40,9 Mb
Release : 1966
Category : Astrodynamics
ISBN : UOM:39015009794325
Author : Patrick Gallais
Publisher : Springer Science & Business Media
Page : 354 pages
File Size : 46,7 Mb
Release : 2007-09-23
Category : Technology & Engineering
ISBN : 9783540736479
Based on a long engineering experience, this book offers a comprehensive and state-of-the-art analysis of aerodynamic and flight mechanic entry topics. This updated edition had new chapters on Re-entry on Mars mission, flight quality, rarefied aerodynamics and re-entry accuracy. In addition, it provides a large set of application exercises and solutions.
Author : Frank J. Regan
Publisher : Unknown
Page : 442 pages
File Size : 54,9 Mb
Release : 1984
Category : Technology & Engineering
ISBN : WISC:89011102993
Author : Frank J. Regan
Publisher : AIAA
Page : 616 pages
File Size : 47,8 Mb
Release : 1993
Category : Space vehicles
ISBN : 160086046X
Author : University of Michigan. Engineering Summer Conferences
Publisher : Unknown
Page : 460 pages
File Size : 48,5 Mb
Release : 1965
Category : Astrodynamics
ISBN : UOM:39015009793210
Author : Ashish Tewari
Publisher : Springer
Page : 136 pages
File Size : 44,8 Mb
Release : 2016-04-22
Category : Technology & Engineering
ISBN : 9783319300221
This book presents flight mechanics of aircraft, spacecraft, and rockets to technical and non-technical readers in simple terms and based purely on physical principles. Adapting an accessible and lucid writing style, the book retains the scientific authority and conceptual substance of an engineering textbook without requiring a background in physics or engineering mathematics. Professor Tewari explains relevant physical principles of flight by straightforward examples and meticulous diagrams and figures. Important aspects of both atmospheric and space flight mechanics are covered, including performance, stability and control, aeroelasticity, orbital mechanics, and altitude control. The book describes airplanes, gliders, rotary wing and flapping wing flight vehicles, rockets, and spacecraft and visualizes the essential principles using detailed illustration. It is an ideal resource for managers and technicians in the aerospace industry without engineering degrees, pilots, and anyone interested in the mechanics of flight.
Author : Ashish Tewari
Publisher : Springer Science & Business Media
Page : 556 pages
File Size : 45,5 Mb
Release : 2007-11-15
Category : Technology & Engineering
ISBN : 9780817644383
This book offers a unified presentation that does not discriminate between atmospheric and space flight. It demonstrates that the two disciplines have evolved from the same set of physical principles and introduces a broad range of critical concepts in an accessible, yet mathematically rigorous presentation. The book presents many MATLAB and Simulink-based numerical examples and real-world simulations. Replete with illustrations, end-of-chapter exercises, and selected solutions, the work is primarily useful as a textbook for advanced undergraduate and beginning graduate-level students.
Author : Claus Weiland
Publisher : Springer Science & Business Media
Page : 300 pages
File Size : 43,7 Mb
Release : 2010-06-29
Category : Technology & Engineering
ISBN : 9783642135835
Themechanicsofspace?ightisan olddiscipline.Itstopicoriginallywasthemotion of planets, moons and other celestial bodies in gravitational ?elds. Kepler’s (1571 - 1630) observations and measurements have led to probably the ?rst mathematical description of planet’s motion. Newton (1642 - 1727) gave then, with the devel- ment of his principles of mechanics, the physical explanation of these motions. Since then man has started in the second half of the 20th centuryto capture ph- ically the Space in the sense that he did develop arti?cial celestial bodies, which he brought into Earth’s orbits, like satellites or space stations, or which he did send to planets or moons of our planetary system, like probes, or by which p- ple were brought to the moon and back, like capsules. Further he developed an advanced space transportation system, the U.S. Space Shuttle Orbiter, which is the only winged space vehicle ever in operation. In the last two and a half decades there were several activities in the world in order to succeed the U.S. Orbiter, like the HERMES project in Europe, the HOPE project in Japan, the X-33, X-34 and X-37 studies and demonstrators in the United States and the joint U.S. - European project X-38. However, all these projects were cancelled. The motion of these vehicles can be described by Newton’s equation of motion.
Author : Paul A. Libby
Publisher : Springer Science & Business Media
Page : 267 pages
File Size : 46,6 Mb
Release : 2013-11-21
Category : Technology & Engineering
ISBN : 9783709154700
In this and a following issue (Vol. VIII, 1962, Fasc. 2-3) of "Astronautica Acta" there will appear the papers presented at the first international symposium sponsored by the International Academy of Astronautics of the International Astronautical Federation. The theme of the meeting was "Space Flight and Re-Entry Trajectories." It was held at Louveciennes outside of Paris on June 19-21, 1961. Sixteen papers by authors from nine countries were presented; attendees numbered from 80 to 100. The organizing committee for the symposium was as follows: Prof. PAUL A. LIBBY, Polytechnic Institute of Brooklyn, U.S.A., Chairman; Prof. LuiGI BROGLIO, University of Rome, Italy; Prof. B. FRAEIJS DE VEUBEKE, University of Liege, Belgium; Dr. D. G. KING-HELE, Royal Aircraft Establishment, Farnborough, Rants, United Kingdom; Prof. J. M. J. KooY, Royal Military School, Breda, Netherlands; Prof. JEAN KovALEVSKY, Bureau des Longitudes, Paris, France; Prof. RuDOLF PESEK, Academy of Sciences, Prague, Czechoslovakia. The detailed arrangements for the meeting were made in a most satisfactory manner by Dr. FRANK J. MALINA, Deputy Director of IAA and Mr. A. R. WEILLER, Acting Secretary of IAA. Prof. THEODORE VON KARMAN, Director of IAA, in his remarks closing the symposium indicated his satisfaction at the interest being shown in "the science of the future." The papers which follow will make a permanent contribution to the literature of this science.
Author : Jack A. White,John A. White
Publisher : Unknown
Page : 56 pages
File Size : 50,9 Mb
Release : 1964
Category : Aerodynamics
ISBN : UIUC:30112106683425
Author : Richard S. Bray,Fred J. Drinkwater
Publisher : Unknown
Page : 34 pages
File Size : 42,7 Mb
Release : 1960
Category : Electronic
ISBN : NASA:31769000455397
Author : Vladimir S Aslanov
Publisher : Butterworth-Heinemann
Page : 420 pages
File Size : 48,6 Mb
Release : 2017-04-22
Category : Technology & Engineering
ISBN : 9780081018743
Rigid Body Dynamics for Space Applications explores the modern problems of spaceflight mechanics, such as attitude dynamics of re-entry and space debris in Earth's atmosphere; dynamics and control of coaxial satellite gyrostats; deployment, dynamics, and control of a tether-assisted return mission of a re-entry capsule; and removal of large space debris by a tether tow. Most space systems can be considered as a system of rigid bodies, with additional elastic and viscoelastic elements and fuel residuals in some cases. This guide shows the nature of the phenomena and explains the behavior of space objects. Researchers working on spacecraft attitude dynamics or space debris removal as well as those in the fields of mechanics, aerospace engineering, and aerospace science will benefit from this book. Provides a complete treatise of modeling attitude for a range of novel and modern attitude control problems of spaceflight mechanics Features chapters on the application of rigid body dynamics to atmospheric re-entries, tethered assisted re-entry, and tethered space debris removal Shows relatively simple ways of constructing mathematical models and analytical solutions describing the behavior of very complex material systems Uses modern methods of regular and chaotic dynamics to obtain results
Author : Vladimir Isaakovich Levantovskiĭ
Publisher : Unknown
Page : 644 pages
File Size : 44,7 Mb
Release : 1972
Category : Astronautics
ISBN : OSU:32435032550022
;Contents: Fundamentals of rocket and space dynamics; Terrestrial flights; Flights to the moon; Interplanetary flights; Space flights.
Author : Anonim
Publisher : UM Libraries
Page : 296 pages
File Size : 47,8 Mb
Release : 1961
Category : Education, Higher
ISBN : UOM:39015078937482
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 114 pages
File Size : 41,6 Mb
Release : 2018-06-13
Category : Electronic
ISBN : 1721103899
This report addresses issues in developing a flight control design for vehicles operating across a broad flight regime and with highly nonlinear physical descriptions of motion. Specifically it addresses the need for reentry vehicles that could operate through reentry from space to controlled touchdown on Earth. The latter part of controlled descent is achieved by parachute or paraglider - or by all automatic or a human-controlled landing similar to that of the Orbiter. Since this report addresses the specific needs of human-carrying (not necessarily piloted) reentry vehicles, it deals with highly nonlinear equations of motion, and then-generated control systems must be robust across a very wide range of physics. Thus, this report deals almost exclusively with some form of dynamic inversion (DI). Two vital aspects of control theory - noninteracting control laws and the transformation of nonlinear systems into equivalent linear systems - are embodied in DI. Though there is no doubt that the mathematical tools and underlying theory are widely available, there are open issues as to the practicality of using DI as the only or primary design approach for reentry articles. This report provides a set of guidelines that can be used to determine the practical usefulness of the technique. Ito, Daigoro and Georgie, Jennifer and Valasek, John and Ward, Donald T. Johnson Space Center