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Dynamics And Control Of Flexible Space Vehicles


Dynamics And Control Of Flexible Space Vehicles
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Dynamics And Control Of Flexible Space Vehicles Revision 1


Dynamics And Control Of Flexible Space Vehicles Revision 1
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Author : P. W. Likins
language : en
Publisher:
Release Date : 1970

Dynamics And Control Of Flexible Space Vehicles Revision 1 written by P. W. Likins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.




Flexible Spacecraft Dynamics Control And Guidance


Flexible Spacecraft Dynamics Control And Guidance
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Author : Leonardo Mazzini
language : en
Publisher: Springer
Release Date : 2015-10-27

Flexible Spacecraft Dynamics Control And Guidance written by Leonardo Mazzini and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-10-27 with Technology & Engineering categories.


This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.



Rigid Flexible Coupling Dynamics And Control Of Flexible Spacecraft With Time Varying Parameters


Rigid Flexible Coupling Dynamics And Control Of Flexible Spacecraft With Time Varying Parameters
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Author : Jie Wang
language : en
Publisher: Springer Nature
Release Date : 2021-09-15

Rigid Flexible Coupling Dynamics And Control Of Flexible Spacecraft With Time Varying Parameters written by Jie Wang and has been published by Springer Nature this book supported file pdf, txt, epub, kindle and other format this book has been release on 2021-09-15 with Technology & Engineering categories.


This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.



Space Vehicle Dynamics And Control


Space Vehicle Dynamics And Control
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Author : Bong Wie
language : en
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Release Date : 2008

Space Vehicle Dynamics And Control written by Bong Wie and has been published by AIAA (American Institute of Aeronautics & Astronautics) this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008 with Science categories.


"Space Vehicle Dynamics and Control, Second Edition" continues to provide a solid foundation in dynamic modeling, analysis, and control of space vehicles featuring detailed sections covering the fundamentals of controlling orbital, attitude, and structural motions of space vehicles. A new Part 5 is a collection of advanced spacecraft control problems and their practical solutions obtained by applying the fundamental principles and techniques emphasized throughout the book.



Dynamics And Control Of Flexible Space Vehicles


Dynamics And Control Of Flexible Space Vehicles
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Author : Peter W. Likins
language : en
Publisher:
Release Date : 1969

Dynamics And Control Of Flexible Space Vehicles written by Peter W. Likins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with Space vehicles categories.




Technology For Large Space Systems


Technology For Large Space Systems
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Author :
language : en
Publisher:
Release Date : 1987

Technology For Large Space Systems written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Large space structures (Astronautics) categories.




Dynamics And Control Of Flexible Spacecraft During And After Slewing Maneuvers


Dynamics And Control Of Flexible Spacecraft During And After Slewing Maneuvers
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-02

Dynamics And Control Of Flexible Spacecraft During And After Slewing Maneuvers written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-02 with categories.


The dynamics and control of slewing maneuvers of NASA Spacecraft COntrol Laboratory Experiment (SCOLE) are analyzed. The control problem of slewing maneuvers of SCOLE is formulated in terms of an arbitrary maneuver about any given axis. The control system is developed for the combined problem of rigid-body slew maneuver and vibration suppression of the flexible appendage. The control problem formulation incorporates the nonlinear dynamical equations derived previously, and is expressed in terms of a two-point boundary value problem utilizing a quadratic type of performance index. The two-point boundary value problem is solved as a hierarchical control problem with the overall system being split in terms of two subsystems, namely the slewing of the entire assembly and the vibration suppression of the flexible antenna. The coupling variables between the two dynamical subsystems are identified and these two subsystems for control purposes are treated independently in parallel at the first level. Then the state-space trajectory of the combined problem is optimized at the second level. Kakad, Yogendra P. Unspecified Center NAG1-535...



Dynamics And Simulation Of Flexible Rockets


Dynamics And Simulation Of Flexible Rockets
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Author : Timothy M. Barrows
language : en
Publisher: Academic Press
Release Date : 2020-12-10

Dynamics And Simulation Of Flexible Rockets written by Timothy M. Barrows and has been published by Academic Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2020-12-10 with Technology & Engineering categories.


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



Dynamics And Control In Modal Space Of Flexible Spacecraft


Dynamics And Control In Modal Space Of Flexible Spacecraft
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Author : Hayrani Öz
language : en
Publisher:
Release Date : 1979

Dynamics And Control In Modal Space Of Flexible Spacecraft written by Hayrani Öz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Space vehicles categories.




Control Of Spacecraft And Aircraft


Control Of Spacecraft And Aircraft
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Author : Arthur E. Bryson Jr.
language : en
Publisher: Princeton University Press
Release Date : 2015-11-03

Control Of Spacecraft And Aircraft written by Arthur E. Bryson Jr. and has been published by Princeton University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2015-11-03 with Technology & Engineering categories.


Here a leading researcher provides a comprehensive treatment of the design of automatic control logic for spacecraft and aircraft. In this book Arthur Bryson describes the linear-quadratic-regulator (LQR) method of feedback control synthesis, which coordinates multiple controls, producing graceful maneuvers comparable to those of an expert pilot. The first half of the work is about attitude control of rigid and flexible spacecraft using momentum wheels, spin, fixed thrusters, and gimbaled engines. Guidance for nearly circular orbits is discussed. The second half is about aircraft attitude and flight path control. This section discusses autopilot designs for cruise, climb-descent, coordinated turns, and automatic landing. One chapter deals with controlling helicopters near hover, and another offers an introduction to the stabilization of aeroelastic instabilities. Throughout the book there is a strong emphasis on the mathematical modeling necessary for designing a good feedback control system. The appendixes summarize analysis of linear dynamic systems, synthesis of analog and digital feedback control, simulation, and modeling of flexible vehicles.