Design of Attitude Control Systems for a Three-axis Stabilized Satellite

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Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (27 download)

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Book Synopsis Design of Attitude Control Systems for a Three-axis Stabilized Satellite by : Joseph Michel Savoie

Download or read book Design of Attitude Control Systems for a Three-axis Stabilized Satellite written by Joseph Michel Savoie and published by . This book was released on 1982 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A flexible attitude control system for three-axis stabilized nanosatellites

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Publisher : Universitätsverlag der TU Berlin
ISBN 13 : 3798329680
Total Pages : 197 pages
Book Rating : 4.7/5 (983 download)

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Book Synopsis A flexible attitude control system for three-axis stabilized nanosatellites by : Gordon, Karsten

Download or read book A flexible attitude control system for three-axis stabilized nanosatellites written by Gordon, Karsten and published by Universitätsverlag der TU Berlin. This book was released on 2018-03-15 with total page 197 pages. Available in PDF, EPUB and Kindle. Book excerpt: This thesis investigates a new concept for the flexible design and verification of an ADCS for a nanosatellite platform. In order to investigate guidelines for the design of a flexible ADCS, observations of the satellite market and missions are recorded. Following these observations, the author formulates design criteria which serve as a reference for the conceptual design of the flexible ADCS. The research of the thesis was carried out during the development of TU Berlin's nanosatellite platform TUBiX20 and its first two missions, TechnoSat and TUBIN. TUBiX20 targets modularity, reuse and dependability as main design goals. Based on the analysis of design criteria for a flexible ADCS, these key design considerations for the TUBiX20 platform were continued for the investigations carried out in this thesis. The resulting concept implements the ADCS as a distributed system of devices complemented by a hardware-independent core application for state determination and control. Drawing on the technique of component-based software engineering, the system is partitioned into self-contained modules which implement unified interfaces. These interfaces specify the state quantity of an input or output but also its unit and coordinate system, complemented by a mathematical symbol for unambiguous documentation. The design and verification process for the TUBiX20 ADCS was also elaborated during the course of this research. The approach targets the gradual development of the subsystem from a purely virtual satellite within a closed-loop simulation to the verification of the fully integrated system on an air-bearing testbed. Finally, the concurrent realization of the investigated concept within the TechnoSat and TUBIN missions is discussed. Starting with the individual ADCS requirements, the scalability of the approach is demonstrated in three stages: from a coarse, but cost- and energy-efficient configuration to realize a technology demonstration mission with moderate requirements (TechnoSat) to a high-performance configuration to support Earth observation missions (TUBIN). Diese Dissertation untersucht ein neues Konzept zur flexiblen Entwicklung und Verifikation eines Lageregelungssystems für eine Nanosatellitenplattform. Als Grundlage für die Erarbeitung eines Leitfadens für die Entwicklung werden zunächst Beobachtung des Satellitenmarkts sowie konkreter Missionen zusammengetragen. Darauf aufbauend formuliert der Autor Entwurfskriterien für die Konzipierung eines flexiblen Lageregelungssystems. Die Dissertation wurde im Rahmen der Entwicklung der TUBiX20 Nanosatellitenplattform und ihrer ersten beiden Missionen, TechnoSat und TUBIN, an der TU Berlin durchgeführt. TUBiX20 verfolgt Modularität, Wiederverwendung und Zuverlässigkeit als Entwicklungsziele. Diese werden unter der Verwendung der vom Autor hergeleiteten Entwurfskriterien in dieser Arbeit im Kontext des Lageregelungssystems verfeinert. Das resultierende Konzept setzt dieses als verteiltes System von Geräten und einem hardware-unabhängigen Software-Kern um. Der Software-Entwurfstechnik Component-based software engineering folgend ist das System in unabhängige Module unterteilt, welche wiederum einheitliche Schnittstellen implementieren. Diese Schnittstellen spezifizieren die Zustandsgrößen für die Ein- und Ausgänge der Module inklusive Einheit, Koordinatensystem und mathematischem Symbol für eine eindeutige Darstellung. Der Entwurfs- und Verifikationsprozess für das TUBiX20 Lageregelungssystem wurde vom Autor im Rahmen der Arbeit untersucht. Hier verfolgt der Ansatz einen schrittweisen übergang von einem virtuellen Satelliten als Simulationsmodell bis hin zur Verifikation des integrierten Systems auf einem Lageregelungsteststand. Abschließend diskutiert die Arbeit die Realisierung des untersuchten Konzepts im Rahmen der Missionen TechnoSat und TUBIN. Beginnend mit den jeweiligen Anforderungen wird die Skalierbarkeit des Ansatzes in drei Stufen demonstriert: von einer groben, aber kosten- und energieeffizienten Konfiguration für eine Technologieerprobungsmission mit moderaten Anforderungen (TechnoSat) bis hin zu einer Konfiguration für hochgenaue Lageregelung als Basis für Erdbeobachtungsmissionen (TUBIN).

Attitude Stabilization for CubeSat

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Publisher : Cambridge Scholars Publishing
ISBN 13 : 152752163X
Total Pages : 190 pages
Book Rating : 4.5/5 (275 download)

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Book Synopsis Attitude Stabilization for CubeSat by : Mohammed Chessab Mahdi

Download or read book Attitude Stabilization for CubeSat written by Mohammed Chessab Mahdi and published by Cambridge Scholars Publishing. This book was released on 2018-11-14 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book explores CubeSat technology, and develops a nonlinear mathematical model of a spacecraft with the assumption that the satellite is a rigid body. It places emphasis on the CubeSat subsystem, orbit dynamics and perturbations, the satellite attitude dynamic and modeling, and components of attitude determination and the control subsystem. The book focuses on the attitude stabilization methods of spacecraft, and presents gravity gradient stabilization, aerodynamic stabilization, and permanent magnets stabilization as passive stabilization methods, and spin stabilization and three axis stabilization as active stabilization methods. It also discusses the need to develop a control system design, and describes the design of three controller configurations, namely the Proportional–Integral–Derivative Controller (PID), the Linear Quadratic Regulator (LQR), and the Fuzzy Logic Controller (FLC) and how they can be used to design the attitude control of CubeSat three-axis stabilization. Furthermore, it presents the design of a suitable attitude stabilization system by combining gravity gradient stabilization with magnetic torquing, and the design of magnetic coils which can be added in order to improve the accuracy of attitude stabilization. The book then investigates, simulates, and compares possible controller configurations that can be used to control the currents of magnetic coils when magnetic coils behave as the actuator of the system.

Design and Simulation of a Three-Axis Stabilized Satellite and Kalman Filter Rate Estimator

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Publisher :
ISBN 13 : 9781423512424
Total Pages : 114 pages
Book Rating : 4.5/5 (124 download)

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Book Synopsis Design and Simulation of a Three-Axis Stabilized Satellite and Kalman Filter Rate Estimator by : John Vitalich

Download or read book Design and Simulation of a Three-Axis Stabilized Satellite and Kalman Filter Rate Estimator written by John Vitalich and published by . This book was released on 2003-06 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design requirements for a small satellite (NPSAT-l) Attitude Determination and Control Subsystem (ADCS) is a three-axis stabilized spacecraft which requires a control attitude of +/- 1,0 degrees and knowledge attitude of +/- 0,1 degree. Several design aspects are considered in development of attitude control systems for a small satellite, such as: spacecraft dynamics, space environment, disturbance torques, orbit type, and spacecraft complexity. The ideal spacecrafts attitude sensor is a rate gyroscope, which provides rate information to the attitude control system In the case of NP SAT- 1, due to budget constraints alternative sensors will be utilized, such as: a three-axis magnetometer, earth sensors, and a Global Positioning System (GPS), A small satellite designed to have a three-axis stabilized, biased momentum system, must have a robust control system, and requires a momentum wheel to provide stiffness to maintain attitude, and magnetic torque rods on each axis. The current design of NPSAT- 1 uses all of these sensors to provide rate information for damping and stability to the control system that requires a complicated attitude control design, The purpose of this attitude control design simulation is to investigate and propose a control law utilizing a single pitch momentum wheel and three magnetic torque rods. A further proposal is to utilize a constant speed momentum wheel to avoid momentum damping and over speed, replace the pitch control with magnetic torquers, and develop a Kalman filter estimator to provide all the required angular rates,

Spacecraft Attitude Determination and Control

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Publisher : Springer Science & Business Media
ISBN 13 : 9400999070
Total Pages : 877 pages
Book Rating : 4.4/5 (9 download)

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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.

Design and Global Analysis of Spacecraft Attitude Control Systems

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Publisher :
ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Design and Global Analysis of Spacecraft Attitude Control Systems by : George Meyer

Download or read book Design and Global Analysis of Spacecraft Attitude Control Systems written by George Meyer and published by . This book was released on 1971 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design of a Three-Axis Stabilized Orion Satellite Using an All-Thruster Attitude Control System

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Publisher :
ISBN 13 :
Total Pages : 116 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Design of a Three-Axis Stabilized Orion Satellite Using an All-Thruster Attitude Control System by : Suzanne M. Dee

Download or read book Design of a Three-Axis Stabilized Orion Satellite Using an All-Thruster Attitude Control System written by Suzanne M. Dee and published by . This book was released on 1988 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: An all-thruster three-axis stabilized attitude control system has been designed for the Naval Postgraduate School (NPS) satellite bus, ORION. The satellite is a cylinder, 19 inches in diameter, 35 inches in length, 250 pounds maximum mass with 32 pounds for payloads. ORION will be ejected from an extended Get-Away-Special (GAS) canister. Launch from any GAS can configure expendable booster or the space shuttle is assumed. The minimization techniques of Pontryagin have been used to derive control laws that support fuel efficient operation. A minimum time cost function is applied in the acquisition phase to reduce rates to acceptable levels. A weighted minimum fuel-time cost function is used during the on-station phase. Bang-Off-Bang control with two switching curves is employed outside of a boundary region. Inside the boundary region, four pulse limit cycle control with time constants on the order of 100 seconds is applied. Satellite, Lightsat, Orion, Naval Postgraduate School, Three axis stabilization, Thruster control, Theses. (mjm).

Design of a Three-Axis Stabilized Orion Satellite Using an All-Thruster Attitude Control System

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Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Design of a Three-Axis Stabilized Orion Satellite Using an All-Thruster Attitude Control System by :

Download or read book Design of a Three-Axis Stabilized Orion Satellite Using an All-Thruster Attitude Control System written by and published by . This book was released on 1988 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An all-thruster three-axis stabilized attitude control system has been designed for the Naval Postgraduate School (NPS) satellite bus, ORION. The satellite is a cylinder, 19 inches in diameter, 35 inches in length, 250 pounds maximum mass with 32 pounds for payloads. ORION will be ejected from an extended Get-Away-Special (GAS) canister. Launch from any GAS can configure expendable booster or the space shuttle is assumed. The minimization techniques of Pontryagin have been used to derive control laws that support fuel efficient operation. A minimum time cost function is applied in the acquisition phase to reduce rates to acceptable levels. A weighted minimum fuel-time cost function is used during the on-station phase. Bang-Off-Bang control with two switching curves is employed outside of a boundary region. Inside the boundary region, four pulse limit cycle control with time constants on the order of 100 seconds is applied. Satellite, Lightsat, Orion, Naval Postgraduate School, Three axis stabilization, Thruster control, Theses. (mjm).

Design and Testing of Three-axis Satellite Attitude Determination and Stabilization Systems that are Based on Magnetic Sensing and Actuation

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Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.:/5 (423 download)

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Book Synopsis Design and Testing of Three-axis Satellite Attitude Determination and Stabilization Systems that are Based on Magnetic Sensing and Actuation by : Mark L. Psiaki

Download or read book Design and Testing of Three-axis Satellite Attitude Determination and Stabilization Systems that are Based on Magnetic Sensing and Actuation written by Mark L. Psiaki and published by . This book was released on 2002 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Peaceful Uses of Automation in Outer Space

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Publisher :
ISBN 13 :
Total Pages : 612 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis Peaceful Uses of Automation in Outer Space by : John A. Aseltine

Download or read book Peaceful Uses of Automation in Outer Space written by John A. Aseltine and published by . This book was released on 1966 with total page 612 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Reusable Reentry Satellite (Rrs) System Design Study. Phase B, Appendix E

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722740832
Total Pages : 46 pages
Book Rating : 4.7/5 (48 download)

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Book Synopsis Reusable Reentry Satellite (Rrs) System Design Study. Phase B, Appendix E by : National Aeronautics and Space Administration (NASA)

Download or read book Reusable Reentry Satellite (Rrs) System Design Study. Phase B, Appendix E written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-11 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study which consisted of a series of design analyses for an Attitude Control System (ACS) to be incorporated into the Re-usable Re-entry Satellite (RRS) was performed. The main thrust of the study was associated with defining the control laws and estimating the mass and power requirements of the ACS needed to meet the specified performance goals. The analyses concentrated on the different on-orbit control modes which start immediately after the separation of the RRS from the launch vehicle. The three distinct on-orbit modes considered for these analyses are as follows: (1) Mode 1 - A Gravity Gradient (GG) three-axis stabilized spacecraft with active magnetic control; (2) Mode 2 - A GG stabilized mode with a controlled yaw rotation rate ('rotisserie') using three-axis magnetic control and also incorporating a 10 N-m-s momentum wheel along the (Z) yaw axis; and (3) Mode 3 - A spin stabilized mode of operation with the spin about the pitch (Y) axis, incorporating a 20 N-m-s momentum wheel along the pitch (Y) axis and attitude control via thrusters. To investigate the capabilities of the different controllers in these various operational modes, a series of computer simulations and trade-off analyses have been made to evaluate the achievable performance levels, and the necessary mass and power requirements. Unspecified Center NAS9-18202; SAIC-11-900286-39...

Spacecraft Dynamics and Control

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Publisher : Cambridge University Press
ISBN 13 : 1139936131
Total Pages : 434 pages
Book Rating : 4.1/5 (399 download)

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Book Synopsis Spacecraft Dynamics and Control by : Marcel J. Sidi

Download or read book Spacecraft Dynamics and Control written by Marcel J. Sidi and published by Cambridge University Press. This book was released on 2000-07-03 with total page 434 pages. Available in PDF, EPUB and Kindle. Book excerpt: Satellites are used increasingly in telecommunications, scientific research, surveillance, and meteorology, and these satellites rely heavily on the effectiveness of complex onboard control systems. This 1997 book explains the basic theory of spacecraft dynamics and control and the practical aspects of controlling a satellite. The emphasis throughout is on analyzing and solving real-world engineering problems. For example, the author discusses orbital and rotational dynamics of spacecraft under a variety of environmental conditions, along with the realistic constraints imposed by available hardware. Among the topics covered are orbital dynamics, attitude dynamics, gravity gradient stabilization, single and dual spin stabilization, attitude maneuvers, attitude stabilization, and structural dynamics and liquid sloshing.

ADCS - Spacecraft Attitude Determination and Control

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Publisher : Elsevier
ISBN 13 : 0323985416
Total Pages : 740 pages
Book Rating : 4.3/5 (239 download)

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Book Synopsis ADCS - Spacecraft Attitude Determination and Control by : Michael Paluszek

Download or read book ADCS - Spacecraft Attitude Determination and Control written by Michael Paluszek and published by Elsevier. This book was released on 2023-04-27 with total page 740 pages. Available in PDF, EPUB and Kindle. Book excerpt: ADCS - Spacecraft Attitude Determination and Control provides a complete introduction to spacecraft control. The book covers all elements of attitude control system design, including kinematics, dynamics, orbits, disturbances, actuators, sensors, and mission operations. Essential hardware details are provided for star cameras, reaction wheels, sun sensors, and other key components. The book explores how to design a control system for a spacecraft, control theory, and actuator and sensor details. Examples are drawn from the author's 40 years of industrial experience with spacecraft such as GGS, GPS IIR, Mars Observer, and commercial communications satellites, and includes historical background and real-life examples. - Features critical details on hardware and the space environment - Combines theory and ready-to-implement practical algorithms - Includes MATLAB code for all examples - Provides plots and figures generated with the included code

Spacecraft Momentum Control Systems

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Publisher : Springer
ISBN 13 : 3319225634
Total Pages : 262 pages
Book Rating : 4.3/5 (192 download)

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Book Synopsis Spacecraft Momentum Control Systems by : Frederick A. Leve

Download or read book Spacecraft Momentum Control Systems written by Frederick A. Leve and published by Springer. This book was released on 2015-10-17 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt: The goal of this book is to serve both as a practical technical reference and a resource for gaining a fuller understanding of the state of the art of spacecraft momentum control systems, specifically looking at control moment gyroscopes (CMGs). As a result, the subject matter includes theory, technology, and systems engineering. The authors combine material on system-level architecture of spacecraft that feature momentum-control systems with material about the momentum-control hardware and software. This also encompasses material on the theoretical and algorithmic approaches to the control of space vehicles with CMGs. In essence, CMGs are the attitude-control actuators that make contemporary highly agile spacecraft possible. The rise of commercial Earth imaging, the advances in privately built spacecraft (including small satellites), and the growing popularity of the subject matter in academic circles over the past decade argues that now is the time for an in-depth treatment of the topic. CMGs are augmented by reaction wheels and related algorithms for steering all such actuators, which together comprise the field of spacecraft momentum control systems. The material is presented at a level suitable for practicing engineers and those with an undergraduate degree in mechanical, electrical, and/or aerospace engineering.

Fast Satellite Attitude Maneuver and Control

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Publisher : Academic Press
ISBN 13 : 0323954561
Total Pages : 280 pages
Book Rating : 4.3/5 (239 download)

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Book Synopsis Fast Satellite Attitude Maneuver and Control by : Dong Ye

Download or read book Fast Satellite Attitude Maneuver and Control written by Dong Ye and published by Academic Press. This book was released on 2022-08-02 with total page 280 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes. It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems. - Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites - Provides a series of the latest results, including, but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites - Comprehensively captures recent advances of theory, technological aspects and applications of fast maneuverer and stabilization control in agile satellites - Addresses research problems in each chapter, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches - Contains comprehensive, up-to-date references, which play an indicative role for further study

Satellite Technology and Its Applications

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Publisher : Notion Press
ISBN 13 :
Total Pages : 766 pages
Book Rating : 4.8/5 (918 download)

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Book Synopsis Satellite Technology and Its Applications by : P. R. K. Chetty

Download or read book Satellite Technology and Its Applications written by P. R. K. Chetty and published by Notion Press. This book was released on 2023-12-27 with total page 766 pages. Available in PDF, EPUB and Kindle. Book excerpt: An authoritative reference on the latest Satellite Technology, including applications, history, evolution, design, descriptions, formulas, calculations and much more. Satellites play a vital role in today’s world and as satellite costs decrease, potential applications grow. Whether you’re a satellite systems engineer, designer, or manager, you need a good, all-purpose reference to this important technology. Now, with Satellite Technology and Its Applications – 3rd Edition, author provides broadened updated coverage of today’s satellite systems, including system data, design formulas and examples, and many other aspects of current spacecraft subsystems. Intended to save you time and effort in your research, this book offers a single source of information related to the design and analysis of satellite systems and their applications. Author’s extensive experience in the U.S., European and Indian space programs gives a wide perspective on this increasingly international scientific endeavor. Satellite design engineers, systems engineers, and managers will find this book to be completely up-to-date, comprehensive and accurate. Regardless of your field of concentration, you’ll discover this comprehensive guide to satellite technology is the most current general reference available.

Control System Design

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Publisher : Courier Corporation
ISBN 13 : 048613511X
Total Pages : 530 pages
Book Rating : 4.4/5 (861 download)

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Book Synopsis Control System Design by : Bernard Friedland

Download or read book Control System Design written by Bernard Friedland and published by Courier Corporation. This book was released on 2012-03-08 with total page 530 pages. Available in PDF, EPUB and Kindle. Book excerpt: Introduction to state-space methods covers feedback control; state-space representation of dynamic systems and dynamics of linear systems; frequency-domain analysis; controllability and observability; shaping the dynamic response; more. 1986 edition.