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Effects Of Structural Flexibility On Launch Vehicle Control Systems
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Book Synopsis Effects of Structural Flexibility on Launch Vehicle Control Systems by : United States. National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Launch Vehicle Control Systems written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Entry Vehicle Control Systems by : United States. National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Entry Vehicle Control Systems written by United States. National Aeronautics and Space Administration and published by . This book was released on 1972 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Spacecraft Control Systems by : National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Spacecraft Control Systems written by National Aeronautics and Space Administration and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Spacecraft Control Systems by : United States. National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Spacecraft Control Systems written by United States. National Aeronautics and Space Administration and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Dynamics and Simulation of Flexible Rockets by : Timothy M. Barrows
Download or read book Dynamics and Simulation of Flexible Rockets written by Timothy M. Barrows and published by Academic Press. This book was released on 2020-12-10 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt: Dynamics and Simulation of Flexible Rockets provides a full state, multiaxis treatment of launch vehicle flight mechanics and provides the state equations in a format that can be readily coded into a simulation environment. Various forms of the mass matrix for the vehicle dynamics are presented. The book also discusses important forms of coupling, such as between the nozzle motions and the flexible body. This book is designed to help practicing aerospace engineers create simulations that can accurately verify that a space launch vehicle will successfully perform its mission. Much of the open literature on rocket dynamics is based on analysis techniques developed during the Apollo program of the 1960s. Since that time, large-scale computational analysis techniques and improved methods for generating Finite Element Models (FEMs) have been developed. The art of the problem is to combine the FEM with dynamic models of separate elements such as sloshing fuel and moveable engine nozzles. The pitfalls that may occur when making this marriage are examined in detail. Covers everything the dynamics and control engineer needs to analyze or improve the design of flexible launch vehicles Provides derivations using Lagrange’s equation and Newton/Euler approaches, allowing the reader to assess the importance of nonlinear terms Details the development of linear models and introduces frequency-domain stability analysis techniques Presents practical methods for transitioning between finite element models, incorporating actuator dynamics, and developing a preliminary flight control design
Book Synopsis Performance Evaluation and Design of Flight Vehicle Control Systems by : Eric T. Falangas
Download or read book Performance Evaluation and Design of Flight Vehicle Control Systems written by Eric T. Falangas and published by John Wiley & Sons. This book was released on 2015-12-02 with total page 432 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this book is to assist analysts, engineers, and students toward developing dynamic models, and analyzing the control of flight vehicles with various blended features comprising aircraft, launch vehicles, reentry vehicles, missiles and aircraft. Graphical methods for analysing vehicle performance Methods for trimming deflections of a vehicle that has multiple types of effectors Presents a parameters used for speedily evaluating the performance, stability, and controllability of a new flight vehicle concept along a trajectory or with fixed flight conditions
Book Synopsis Solid Propellant Grain Structural Integrity Analysis by : James S. Noel
Download or read book Solid Propellant Grain Structural Integrity Analysis written by James S. Noel and published by . This book was released on 1973 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Practical Design of Flight Control Systems for Launch Vehicles and Missiles by : N.V. Kadam
Download or read book Practical Design of Flight Control Systems for Launch Vehicles and Missiles written by N.V. Kadam and published by Allied Publishers. This book was released on 2009-06-15 with total page 380 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book gives in a concise and easy to understand form the various aspects of Practical Design of Flight Control Systems for Launch Vehicles and Missiles. It covers almost every aspect of Flight Control System Design which a designer would like to know, such as mission considerations, control requirements for various segments of the flight trajectory and different types of control effectors. It further gives generalized equations of motion with a novel method of incorporating structural flexibility and propellant sloshing which does not require rederivation, and very easy and common sense approach to deriving slosh and gimballed engine dynamic equations. Subsequently it gives the control system configurations, power plant sizing, loop design for linearised system and detailed analysis and design of on-off reaction control systems. It also covers various software features which are necessary for actual implementation of the design in flight missions, robustness features to avoid malfunctioning in some circumstances, design validation aspects including end-to-end sign checks and describes some flight experiences which called for design updates. The book is unique for its strong practical flavour and is directly useful to the working engineers in the field and post graduate students in Aerospace Engineering.
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 Liquid Rocket Actuators and Operators by : James G. Absalom
Download or read book Liquid Rocket Actuators and Operators written by James G. Absalom and published by . This book was released on 1973 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Surface Atmospheric Extremes by : Goddard Space Flight Center
Download or read book Surface Atmospheric Extremes written by Goddard Space Flight Center and published by . This book was released on 1974 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Commercial Satellite Launch Vehicle Attitude Control Systems Design and Analysis (H-infinity, Loop Shaping, and Coprime Approach) by : Chong Hun Kim
Download or read book Commercial Satellite Launch Vehicle Attitude Control Systems Design and Analysis (H-infinity, Loop Shaping, and Coprime Approach) written by Chong Hun Kim and published by Lulu.com. This book was released on 2007 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is written for aerospace engineers who have completed their BS degree and are interested in the design and analysis of rocket attitude control systems. It introduces a new approach to the design, characterized by its robustness. Current LV attitude control systems are designed based on classical SISO control theory, and they lack robustness. The theory used here truly offers a technique that enables us to design control systems that are reasonably insensitive to math modeling errors and can withstand disturbances such as gust, and in addition it doesn’t need external states estimator, such as Kalman filtering. Extensive simulation results, which demonstrate the effectiveness of this approach, are presented in this book. Basic rocket theory and a concept of H-infinity control system design technique are explained for those who are new in these fields of study.
Book Synopsis Advances in Structural Vibration by : Subashisa Dutta
Download or read book Advances in Structural Vibration written by Subashisa Dutta and published by Springer Nature. This book was released on 2020-10-11 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book consists of selected and peer-reviewed papers presented at the 13th International Conference on Vibration Problems (ICOVP 2017). The topics covered in this book include different structural vibration problems such as dynamics and stability under normal and seismic loading, and wave propagation. The book also discusses different materials such as composite, piezoelectric, and functionally graded materials for improving the stiffness and damping properties of structures. The contents of this book can be useful for beginners, researchers and professionals interested in structural vibration and other allied fields.
Book Synopsis Structural Design Criteria Applicable to a Space Shuttle by :
Download or read book Structural Design Criteria Applicable to a Space Shuttle written by and published by . This book was released on 1972 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis System Analysis Approach to Deriving Design Criteria (Loads) for Space Shuttle and Its Payloads. Volume 2: Typical Examples by : Robert Samuel Ryan
Download or read book System Analysis Approach to Deriving Design Criteria (Loads) for Space Shuttle and Its Payloads. Volume 2: Typical Examples written by Robert Samuel Ryan and published by . This book was released on 1981 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Modern Course in Aeroelasticity by : Howard C. Curtiss Jr.
Download or read book A Modern Course in Aeroelasticity written by Howard C. Curtiss Jr. and published by Springer Science & Business Media. This book was released on 2013-11-11 with total page 575 pages. Available in PDF, EPUB and Kindle. Book excerpt: Areader who achieves a substantial command of the material con tained in this book should be able to read with understanding most of the literature in the field. Possible exceptions may be certain special aspects of the subject such as the aeroelasticity of plates and sheIls or the use of electronic feedback control to modify aeroelastic behavior. The first author has considered the former topic in aseparate volume. The latter topic is also deserving of aseparate volume. In the first portion of the book the basic physical phenomena of divergence, control surface eflectiveness, flutter and gust response of aeronautical vehicles are treated. As an indication of the expanding scope of the field, representative examples are also drawn from the non aeronautical literature. To aid the student who is encountering these phenomena for the first time, each is introduced in the context of a simple physical model and then reconsidered systematicaIly in more compli cated models using more sophisticated mathematics.
Book Synopsis A Modern Course in Aeroelasticity by : E.H. Dowell
Download or read book A Modern Course in Aeroelasticity written by E.H. Dowell and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 724 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aeroelasticity is the study of flexible structures situated in a flowing fluid. Its modern origins are in the field of aerospace engineering, but it has now expanded to include phenomena arising in other fields such as bioengineering, civil engineering, mechanical engineering and nuclear engineering. The present volume is a teaching text for a first, and possibly second, course in aeroelasticity. It will also be useful as a reference source on the fundamentals of the subject for practitioners. In this third edition, several chapters have been revised and three new chapters added. The latter include a brief introduction to `Experimental Aeroelasticity', an overview of a frontier of research `Nonlinear Aeroelasticity', and the first connected, authoritative account of `Aeroelastic Control' in book form. The authors are drawn from a range of fields including aerospace engineering, civil engineering, mechanical engineering, rotorcraft and turbomachinery. Each author is a leading expert in the subject of his chapter and has many years of experience in consulting, research and teaching.
