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Author : Gerald Cook
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.X/5 (4 download)
Download or read book Body fixed missile analysis written by Gerald Cook and published by . This book was released on 1981 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John K. Kryvoruka
Publisher :
ISBN 13 :
Total Pages : 64 pages
Book Rating : 4.:/5 (126 download)
Download or read book Analysis of the Motion of Free-flight Missiles from Body-fixed Sensors written by John K. Kryvoruka and published by . This book was released on 1970 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Thomas Lee Cost
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Analysis of Missile Yaw, Pitch, Roll and Bending Motion from Body-fixed Sensors written by Thomas Lee Cost and published by . This book was released on 1982 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Rafael Yanushevsky
Publisher : CRC Press
ISBN 13 : 142006228X
Total Pages : 242 pages
Book Rating : 4.4/5 (2 download)
Download or read book Modern Missile Guidance written by Rafael Yanushevsky and published by CRC Press. This book was released on 2007-09-20 with total page 242 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written by an expert with more than 30 years of experience, Modern Missile Guidance contains new analytical results, obtained by the author, that can be used for analysis and design of missile guidance and control systems. This book covers not just new methods nor is it merely a compilation of older methods, although it includes both. The book disc
Author : Wayne H. Hathaway
Publisher :
ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (227 download)
Download or read book Aeroballistic Range Data Analysis for Nonsymmetric Configurations written by Wayne H. Hathaway and published by . This book was released on 1976 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: A model (equations of motion) has been developed which is capable of computing the six-degree-of-freedom trajectory of a nonsymmetric missile. The forces and moments considered to be acting on the missile are described in a body-fixed coordinate system. The model has been incorporated in a data correlation technique using differential corrections and least-squares theory. A system of five computer programs was developed for complete analysis of ballistic spark range data on a nonsymmetric missile. These are to be used for analysis of data gathered in the USAF Aeroballistic Research Facility, Eglin AFB. The model and data correlation technique were used to anlayze ballistic spark range data on two elliptic cones. Individual and simultaneous reductions resulted in probable errors of fit approximately equal to the accuracy of the data. The results of these reductions are presented.
Author : Marvin E. Sellers
Publisher :
ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.3/5 (91 download)
Download or read book Static Stability Test of Three Elliptic Missile Body Configurations written by Marvin E. Sellers and published by . This book was released on 1985 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : G. R. Gomillion
Publisher :
ISBN 13 :
Total Pages : 404 pages
Book Rating : 4.3/5 (91 download)
Download or read book A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models with and Without Tail Fins and Wings written by G. R. Gomillion and published by . This book was released on 1976 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document contains a compilation of aerodynamic data for the Martin Generalized Research Model, which is a composite of several body, wing, and tail fin configurations typical of missile applications. The model variations included five body configurations, three wing configurations at various body locations, and 15 tail fin configurations. Static stability and tail fin loads data are presented in tabulated and plotted form for a Mach number range from 0.20 to 4.63 over an angle-of-attack range from -6 to 60 deg and a sideslip angle range from -20 to 20 deg for the body-alone configurations, body-wing configurations, and the body-wing-tail fin configurations. In addition, the tail fin configurations were tested using the reflection plane technique, and the resulting fin loads data are presented for a Mach number range of 0.80 to 2.16 over an angle-of-attack range from 0 to 210 deg. Volume I contains the narrative and selected plotted data. (Author).
Author : Larry D. Johnson
Publisher :
ISBN 13 :
Total Pages : 137 pages
Book Rating : 4.:/5 (227 download)
Download or read book Body Fixed Guidance and Control Concept and Design Study written by Larry D. Johnson and published by . This book was released on 1973 with total page 137 pages. Available in PDF, EPUB and Kindle. Book excerpt: The primary purpose of a missile guidance and control system is to influence the flight of the missile such that the terminal miss distance between the missile and the target is eliminated or reduced to an acceptable value. The purpose of this program was to determine the feasibility of a simple, low-cost, body-fixed semi-active laser seeker and reaction jet control system.
Author :
Publisher :
ISBN 13 :
Total Pages : 244 pages
Book Rating : 4.:/5 (3 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1990 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Philip N. Jenkins
Publisher :
ISBN 13 :
Total Pages : 222 pages
Book Rating : 4.3/5 (91 download)
Download or read book Missile Dynamics Equations for Guidance and Control Modeling and Analysis written by Philip N. Jenkins and published by . This book was released on 1976 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents some techniques used in deriving the equations of motion of a missile for a six-degree-of-freedom (6-DOF) simulation. Several forms of the equations are developed, and their implementation is discussed. Specific emphasis is placed on showing the interrelation of the equation forms currently in use by showing their development from the basic laws. This report is meant to serve as a primer for new engineers and as a reference for all engineers involved in missile flight simulation.
Author : G. R. Gomillion
Publisher :
ISBN 13 :
Total Pages : 1798 pages
Book Rating : 4.3/5 (91 download)
Download or read book A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models with and Without Tail Fins and Wings written by G. R. Gomillion and published by . This book was released on 1976 with total page 1798 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William J. Monta
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)
Download or read book Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : G. R. Gomillion
Publisher :
ISBN 13 :
Total Pages : 1950 pages
Book Rating : 4.3/5 (91 download)
Download or read book A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models with and Without Tail Fins and Wings written by G. R. Gomillion and published by . This book was released on 1976 with total page 1950 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Marvin E. Sellers
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.3/5 (91 download)
Download or read book Pressure Test of Three Elliptic Missile Body Configuratins written by Marvin E. Sellers and published by . This book was released on 1985 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Rudolf F. Glaser
Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (31 download)
Download or read book Vibration and Stability Analysis of Compressed Rocket Vehicles written by Rudolf F. Glaser and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Rafael Yanushevsky
Publisher : CRC Press
ISBN 13 : 1439850968
Total Pages : 373 pages
Book Rating : 4.4/5 (398 download)
Download or read book Guidance of Unmanned Aerial Vehicles written by Rafael Yanushevsky and published by CRC Press. This book was released on 2011-03-29 with total page 373 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written by an expert with more than 30 years of experience, Guidance of Unmanned Aerial Vehicles contains new analytical results, taken from the author's research, which can be used for analysis and design of unmanned aerial vehicles guidance and control systems. This book progresses from a clear elucidation of guidance laws and unmanned aerial veh
Author : Farhan A. Faruqi
Publisher : John Wiley & Sons
ISBN 13 : 1119168503
Total Pages : 213 pages
Book Rating : 4.1/5 (191 download)
Download or read book Differential Game Theory with Applications to Missiles and Autonomous Systems Guidance written by Farhan A. Faruqi and published by John Wiley & Sons. This book was released on 2017-03-10 with total page 213 pages. Available in PDF, EPUB and Kindle. Book excerpt: Differential Game Theory with Applications to Missiles and Autonomous Systems explains the use of differential game theory in autonomous guidance and control systems. The book begins with an introduction to the basic principles before considering optimum control and game theory. Two-party and multi-party game theory and guidance are then covered and, finally, the theory is demonstrated through simulation examples and models and the simulation results are discussed. Recent developments in the area of guidance and autonomous systems are also presented. Key features: Presents new developments and how they relate to established control systems knowledge. Demonstrates the theory through simulation examples and models. Covers two-party and multi-party game theory and guidance. Accompanied by a website hosting MATLAB® code. The book is essential reading for researchers and practitioners in the aerospace and defence industries as well as graduate students in aerospace engineering.
