Dynamic Modeling Guidance and Control of Homing Missiles

Dynamic Modeling  Guidance  and Control of Homing Missiles

As a complementary part of the work, the design of a target state estimator is made as a first order fading memory filter. Finally, the entire guidance and control system is built by integrating all the models mentioned abo.

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ISBN: OCLC:611693701

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DYNAMIC MODELING, GUIDANCE, AND CONTROL OF HOMING MISSILES ÖZKAN, Bülent Ph. D., Department of Mechanical Engineering Supervisor: Prof. Dr. M. Kemal ÖZGÖREN Co-Supervisor: Dr. Gökmen MAHMUTYAZICIOÐLU September 2005, 236 pages In this study, the dynamic modeling, guidance, and control of a missile with two relatively rotating parts are dealt with. The two parts of the missile are connected to each other by means of a roller bearing. In the first part of the study, the governing differential equations of motion of the mentioned missile are derived. Then, regarding the relative rotation between the bodies, the aerodynamic model of the missile is constructed by means of the Missile Datcom software available in TÜBÝTAK-SAGE. After obtaining the required aerodynamic stability derivatives using the generated aerodynamic data, the necessary transfer functions are determined based on the equations of motion of the missile. Next, the guidance laws that are considered in this study are formulated. Here, the Linear Homing Guidance and the Parabolic Homing Guidance laws are introduced as alternatives to the Proportional Navigation Guidance law. On this occasion, the spatial derivation of the Proportional Navigation Guidance law is also done. Afterwards, the roll, pitch and yaw autopilots are designed using the determined transfer functions. As the roll autopilot is constructed to regulate the roll angle of the front body of the missile which is the controlled part, the pitch and yaw autopilots are designed to realize the command signals generated by the guidance laws. The guidance commands are in the form of either the lateral acceleration components or the flight path angles of the missile. Then, the target kinematics is modeled for a typical surface target. As a complementary part of the work, the design of a target state estimator is made as a first order fading memory filter. Finally, the entire guidance and control system is built by integrating all the models mentioned abo.
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Applied Min max Approach to Missile Guidance and Control

Applied Min max Approach to Missile Guidance and Control

This book is concerned with dynamical systems under a large uncertainty, and uses a min-max approach to achieve worst-case design. The book consists of two parts. The first part deals with robust control.

Author: Shaul Gutman

Publisher: Amer Inst of Aeronautics &

ISBN: UOM:39015062445476

Category: Technology & Engineering

Page: 298

View: 813

This book is concerned with dynamical systems under a large uncertainty, and uses a min-max approach to achieve worst-case design. The book consists of two parts. The first part deals with robust control. It begines by developing linear controls to achieve relative stability (pole clustering) under parameter uncertainty. Surprisingly, the largest robustness radius in the parameter space is sometimes discontinuous (fragile) with respect to the control parameters. Then, the book discusses the control of nonlinear uncertain systems under matching conditions. The second part uses differential games to develop optimal guidance for homing missiles against maneuvering targets. The target maneuver is bounded, but otherwise, arbitrary. Using miss distance as the cost, the book develops closed form guidance laws, as well as miss distance formulae. In this way, the control loop (autopilot) and the guidance loop are coupled. A parameter study reveals the basic difference between minimum phase (canards) and non minimum phase (tail control) missiles. It also shows the influence of the autopilot parameters on the miss distance.
Categories: Technology & Engineering

Missile Guidance and Pursuit

Missile Guidance and Pursuit

The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite.

Author: N A Shneydor

Publisher: Elsevier

ISBN: 9781782420590

Category: Technology & Engineering

Page: 266

View: 995

The continuing evolving capability of guided weapons demands ever more knowledge of their development. This modern and comprehensive book covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer. The text studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process. Mathematics at first-year university level is the only prerequisite. Acquaintance with feedback control theory would be helpful to the reader. Covers the control aspect of guidance of missiles, torpedoes, robots, and even animal predators, from the viewpoint of the pursuer Studies trajectories, zones of interception, the required manoeuvre effort, time of flight, launch envelopes, and stability of the guidance process
Categories: Technology & Engineering

Modern Missile Guidance

Modern Missile Guidance

The design procedure to modernize the existing missile guidance and control
systems will enable designers to modify the ... Palumbo, N., Reardon, B., and
Blauwkamp, R., Integrated guidance and control for homing missiles, Johns
Hopkins ...

Author: Rafael Yanushevsky

Publisher: CRC Press

ISBN: 142006228X

Category: Technology & Engineering

Page: 240

View: 893

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 discusses, in a logical progression, with its clear elucidation of the guidance laws, the entire field from missile dynamics to modeling and testing missile guidance and control systems. In contrast to existing books that discuss very simple and often unrealistic guidance system models, this book presents missile guidance models that describe more precisely the dynamics of the missile flight control system, making analytical results more effective in practice. The analysis of missile guidance system models in the time-domain and in the frequency-domain allows the generation of different guidance laws that supplement each other. Taking modern, rigorous approach that leads to improved performance in missile guidance applications, the book examines new guidance laws, and corresponding algorithms for generating and testing these laws, and includes effective new software programs developed by the author. The author provides an innovative presentation of the theoretical aspects of modern missile guidance that quite possibly cannot be found in any other book. It delineates new ideas that, once crystallized, will significantly improve missile systems performance.
Categories: Technology & Engineering

Missile Guidance

Missile Guidance

Author: John Clemow

Publisher:

ISBN: STANFORD:36105030335140

Category: Guidance systems (Flight)

Page: 87

View: 495

Categories: Guidance systems (Flight)

Basics of Missile Guidance and Space Techniques

Basics of Missile Guidance and Space Techniques

This volume covers guidanec techniques, control and guidance, radio and radar command, guide beam, doppler and homing techniques, gryoscopic fundamentals, inertial and celestial navigation, computer applications, and actuators.

Author: Marvin Hobbs

Publisher: Wildside Press LLC

ISBN: 9781434421258

Category: Science

Page: 154

View: 188

This volume covers guidanec techniques, control and guidance, radio and radar command, guide beam, doppler and homing techniques, gryoscopic fundamentals, inertial and celestial navigation, computer applications, and actuators.
Categories: Science

Principles of Guided Missiles and Nuclear Weapons

Principles of Guided Missiles and Nuclear Weapons

Fundamentals of missile and nuclear weapons systems are presented in this book which is primarily prepared as the second text of a three-volume series for students of the Navy Reserve Officers' Training Corps and the Officer Candidate ...

Author: United States. Bureau of Naval Personnel

Publisher:

ISBN: UIUC:30112077982848

Category: Guided missiles

Page: 366

View: 230

Fundamentals of missile and nuclear weapons systems are presented in this book which is primarily prepared as the second text of a three-volume series for students of the Navy Reserve Officers' Training Corps and the Officer Candidate School. Following an introduction to guided missiles and nuclear physics, basic principles and theories are discussed with a background of the factors affecting missile flight, airframes, missile propulsion systems, control components and systems, missile guidance, guided missile ships and systems, nuclear weapons, and atomic warfare defense. In the area of missile guidance, further explanations are made of command guidance, beam-rider methods, homing systems, preset guidance, and navigational guidance systems. Effects of nuclear weapons are also described in categories of air, surface, subsurface, underwater, underground, and high-altitude bursts as well as various kinds of damages and injuries. Besides illustrations for explanation purposes, a table of atomic weights and a glossary of general terms are provided in the appendices.
Categories: Guided missiles

Missile Guidance and Control Systems

Missile Guidance and Control Systems

1, January 1989, M.: An Engineering Approach to Optimal Control and Estimation
Theory, & Sons, Inc., New York, NY, 1996. ... 251–263. arget Adaptive Guidance
for Passive Homing Missiles, IEEE Transactions and Electronic Systems, Vol.

Author: George M. Siouris

Publisher: Springer Science & Business Media

ISBN: 9780387218168

Category: Technology & Engineering

Page: 666

View: 527

Airborne Vehicle Guidance and Control Systems is a broad and wide- angled engineering and technological area for research, and continues to be important not only in military defense systems but also in industrial process control and in commercial transportation networks such as various Global Positioning Systems (GPS). The book fills a long-standing gap in the literature. The author is retired from the Air Force Institute and received the Air Force's Outstanding Civilian Career Service Award.
Categories: Technology & Engineering

Advances in Missile Guidance Control and Estimation

Advances in Missile Guidance  Control  and Estimation

S. N. Balakrishnan, D. T. Stansbery, J. H. Evers, and J. R. Cloutier. Analytical
Guidance Laws and Integrated Guidance/Autopilot for Homing Missiles. In IEEE
International Conference on Control Applications, pp. 27–32, 1993. 6. G. W.
Cherry.

Author: S.N. Balakrishnan

Publisher: CRC Press

ISBN: 9781420083149

Category: Technology & Engineering

Page: 720

View: 200

Stringent demands on modern guided weapon systems require new approaches to guidance, control, and estimation. There are requirements for pinpoint accuracy, low cost per round, easy upgrade paths, enhanced performance in counter-measure environments, and the ability to track low-observable targets. Advances in Missile Guidance, Control, and Estimat
Categories: Technology & Engineering

Missile Guidance

Missile Guidance

Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online.

Author: Source Wikipedia

Publisher: University-Press.org

ISBN: 1230484299

Category:

Page: 58

View: 871

Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. Pages: 56. Chapters: Active radar homing, Advanced Inertial Reference Sphere, All-aspect, Beam riding, Command guided, D-17B, D-37C, D37D, Fire-and-forget, Global Positioning System, GPS augmentation, IBM AN/FSQ-7 Combat Direction Central, Inertial navigation system, Infrared homing, Laser designator, Laser guidance, Line-of-sight (missile), MCLOS, MISTRAM, Project Pigeon, Proportional navigation, Pursuit guidance, Q-guidance, SACLOS, SAGEM Sigma 30, Semi-active radar homing, Staring array, TERCOM, TERPROM, Track-via-missile, UDOP, Wire-guided missile. Excerpt: The Global Positioning System (GPS) is a space-based satellite navigation system that provides location and time information in all weather conditions, anywhere on or near the Earth where there is an unobstructed line of sight to four or more GPS satellites. The system provides critical capabilities to military, civil and commercial users around the world. It is maintained by the United States government and is freely accessible to anyone with a GPS receiver. The GPS project was developed in 1973 to overcome the limitations of previous navigation systems, integrating ideas from several predecessors, including a number of classified engineering design studies from the 1960s. GPS was created and realized by the U.S. Department of Defense (DoD) and was originally run with 24 satellites. It became fully operational in 1994. Roger L. Easton is generally credited as its inventor. Advances in technology and new demands on the existing system have now led to efforts to modernize the GPS system and implement the next generation of GPS III satellites and Next Generation Operational Control System (OCX). Announcements from the Vice President and the White House in 1998 initiated these changes. In 2000, U.S. Congress authorized the modernization effort, GPS III. In addition to GPS, other...
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Guided Weapon Control Systems

Guided Weapon Control Systems

Indhold: The Performance of Target Trackers; Missile Servos; Missile Control Methods; Aerodynamic Derivatives and Aerodynamic Transfer Functions; Missile Instruments; Autopilot Design; Line of Sight Guidance Loops; Homing Heads and some ...

Author: P. Garnell

Publisher: Pergamon

ISBN: 0080196918

Category: Guided missiles

Page: 282

View: 427

Indhold: The Performance of Target Trackers; Missile Servos; Missile Control Methods; Aerodynamic Derivatives and Aerodynamic Transfer Functions; Missile Instruments; Autopilot Design; Line of Sight Guidance Loops; Homing Heads and some Associated Stability Problems; Proportional Navigation and Homing Guidance Loops; Wiener Filter Theory Applied to Guidance Loops Design; Modern Control Theory Applied to Guidance Loop Design; Kalman Filters.
Categories: Guided missiles

Advances in Science and Engineering

Advances in Science and Engineering

References [1] Nesline, F.W. and Zarchan, P. “A new look at classical vs. modern
homing missile guidance,” in:Journal of Guidance and Control, Vol. 4(1981),p. 78
-85. [2] Lin, C.F,in: Modern Navigation, Guidance, and Control Processing, ...

Author: Zhi Lin Zhu

Publisher: Trans Tech Publications Ltd

ISBN: 9783038135234

Category: Technology & Engineering

Page: 1080

View: 284

This special collection of peer reviewed papers focuses on frontier topics in the fields of theoretical and applied engineering and science. Volume is indexed by Thomson Reuters CPCI-S (WoS). The 170 selected high-quality papers are grouped under seven rubrics: Automation, Advanced Intelligence and Bio-informatics, Electronic & Energy, Communication, Image Processing and Information, Mechanical Engineering, Other Applications.
Categories: Technology & Engineering

Tactical and Strategic Missile Guidance

Tactical and Strategic Missile Guidance

Previous editions of the text have shown that intentional or unintentional spiraling maneuvers by a tactical ballistic missile can make it particularly difficult for a pursuing missile to hit.

Author: Paul Zarchan

Publisher: Amer Inst of Aeronautics &

ISBN: UOM:39015069193954

Category: Science

Page: 888

View: 524

The fifth edition of this best-selling title has three new chapters on important topics related to improving missile guidance performance and several important new concepts in the Appendix. The first new chapter presents several alternative ways of developing guidance laws numerically. These techniques can be used to derive more advanced guidance laws when the missile guidance system dynamics become very complex. An example is presented showing the advantages of a new advanced guidance law over more conventional guidance laws. Previous editions of the text have shown that intentional or unintentional spiraling maneuvers by a tactical ballistic missile can make it particularly difficult for a pursuing missile to hit.
Categories: Science

NASA Technical Memorandum

NASA Technical Memorandum

MISSILE CONTROL UF MISSILE GUIDANCE MISSILE STABILIZATION RT
ACTUATORS ANALOG COMPUTERS ... RIDER GUIDANCE CONTROL
DIRECTIONAL CONTROL FLIGHT CONTROL GROUND BASED CONTROL
HOMING LASER ...

Author: United States. National Aeronautics and Space Administration

Publisher:

ISBN: UOM:39015022351913

Category: Aeronautics

Page:

View: 440

Categories: Aeronautics

Knowledge Based Intelligent Information and Engineering Systems 1

Knowledge Based Intelligent Information and Engineering Systems 1

Guidance. in. the. Homing. Missiles. Mustafa Resa Becan and Ahmet Kuzucu
System Dynamics and Control Unit, Mechanical Engineering Faculty ... Noise
effects in homing missile guidance must be reduced to get an accurate control.

Author: Vasile Palade

Publisher: Springer Science & Business Media

ISBN: 9783540408031

Category: Business & Economics

Page: 1476

View: 179

The two volumes LNAI 2773 and LNAI 2774 constitute the refereed proceedings of the 7th International Conference on Knowledge-Based Intelligent Information and Engineering Systems, KES 2003, held in Oxford, UK in September 2003.The 390 revised papers and poster papers presented were carefully reviewed and selected from numerous submissions. Among the areas covered are knowledge-based systems, neural computing, fuzzy logic, uncertainty, machine learning, soft computing, agent systems, intelligent agents, data mining, knowledge discovery, hybrid intelligent systems, natural language processing, information retrieval, Web applications, case-based reasoning, evolutionary computing, signal processing, ontologies, decision making, human-computer interaction, intelligent user interfaces, neuroscience, intelligent agents, biocomputing, etc.
Categories: Business & Economics

Compound Control Methodology for Flight Vehicles

Compound Control Methodology for Flight Vehicles

Proportional navigation (PN) has attracted a amount of interest in the missile
interception and design of guidance laws due to the high effectiveness and
simple ... In [284], a robust H∞ guidance law is proposed for homing missiles.

Author: Yuanqing Xia

Publisher: Springer

ISBN: 9783642368417

Category: Technology & Engineering

Page: 260

View: 152

“Compound Control Methodology for Flight Vehicles” focuses on new control methods for flight vehicles. In this monograph, the concept of compound control is introduced. It is demonstrated that both Sliding Mode Control (SMC) and Active Disturbance Rejection Control (ADRC) have their own advantages and limitations, i.e., chattering of SMC and the observability of extended state observer (ESO), respectively. It is shown that compound control combines their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle control.
Categories: Technology & Engineering