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: 997

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 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: 312

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: 179

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

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: 101

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

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: 446

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

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: 529

Categories: Aeronautics

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: 409

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

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: 203

“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

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: 532

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

Bank to turn Control Technology Survey for Homing Missiles

Bank to turn Control Technology Survey for Homing Missiles

R . A . Gardiner , " Flight Test of a Roll - Control Homing System , " NACA
Conference on Automatic Stability and ... to - Turn Steering for Highly
Maneuverable Missiles , " Proceedings of the AIAA Guidance and Control
Conference , Aug .

Author: Frederick William Riedel

Publisher:

ISBN: NASA:31769000504384

Category: Guided missiles

Page: 37

View: 832

Categories: Guided missiles

Proceedings

Proceedings

If 0.5 < n < 1 , then it is easy to find a " bias " that guarantees that at least every
second antisurface missile will be intercepted and destroyed ... Gutman , S. : " On
Optimal Guidance for Homing Missiles " , Journal of Guidance and Control , Vol .

Author: American Automatic Control Council

Publisher:

ISBN: 0780324463

Category:

Page:

View: 396

Categories:

Naval Weapons Systems and the Contemporary Law of War

Naval Weapons Systems and the Contemporary Law of War

The main disadvantage is that guidance accuracy diminishes as distance from
the director increases . Homing or autonomous guidance systems control the
missile's flight by employing a device that reacts to some feature or aspect of the
 ...

Author: James J. Busuttil

Publisher: Oxford University Press

ISBN: 0198265743

Category: Law

Page: 249

View: 661

This book provides the first comprehensive critical analysis of the regulation of naval weapons during armed conflict. It examines the experience this century with the use of naval mines, submarines and anti-ship missiles, the three main naval weapons. The sources of international law relevant to an assessment of the law, that is the extant conventions, state practice, military manuals, war crimes prosecutions, and the opinions of publicists, are each extensively examined so that a clear picture of the law emerges. The book examines the impact of agreements drawn up in peacetime on wartime conduct and focuses on the growth of law through customary practice. While stating the law as it is today, it also provides suggestions for the practical development of the law.
Categories: Law

Modern Navigation Guidance and Control Processing

Modern Navigation  Guidance  and Control Processing

Price , C . F . AND R . S . WARREN , “ Performance Evaluation of Homing
Guidance Laws for Tactical Missiles , ” The Analytical Sciences Corp . , Rept . No
. TR - 170 - 4 , January 1973 . Radio TECHNICAL COMMISSION FOR
AERONAUTICS ...

Author: Ching-Fang Lin

Publisher: Prentice Hall Series in Advanc

ISBN: UOM:39015024961677

Category: Technology & Engineering

Page: 671

View: 797

M->CREATED
Categories: Technology & Engineering

Guidance and Control 1989

Guidance and Control 1989

Proceedings of the Annual Rocky Mountain Guidance and Control Conference
Held February 4-8, 1989, Keystone, Colorado Robert D. ... Yeuh , W . R . , and C .
F . Lin , " Optimal Controller for Homing Missile , " Journal of Guidance , Vol .

Author: Robert D. Culp

Publisher: Amer Astronautical Society

ISBN: UCSD:31822004186789

Category: Space vehicles

Page: 691

View: 222

Categories: Space vehicles

Theory and Application of Digital Control

Theory and Application of Digital Control

Theory and Application of Digital Control New Delhi, India 1982 MODEL
SIMPLIFICATION AND DIGITAL DESIGN OF MULTIVARIABLE ... University of
Houston, Houston, Texas, USA **Guidance & Control Directorate, U.S. Army
Missile Command, Redstone Arsenal, Alabama, USA Abstract. ... Aircraft
autopilots and terminal homing missiles are typical examples (Yates and Co-
workers, 1976).

Author: A. K. Mahalanabis

Publisher: Elsevier

ISBN: 9781483153773

Category: Technology & Engineering

Page: 704

View: 940

Theory and Application of Digital Control contains the proceedings of the IFAC Symposium held at New Delhi, India on January 5-7, 1982. This book particularly presents the texts of the five plenary talks and the 110 papers of the symposium. This book organizes the papers into 109 chapters, with nearly one-third of the papers focus on digital control, particularly, software and hardware of control using microcomputers; computer-aided design; and adaptive control and modeling for digital control. Another set of papers deal with several applications of digital control techniques in solving interesting problems of socio economic systems, electrical power systems, bio systems, and artificial satellites. The reader will benefit hugely from the topics in this book that span several important theoretical and applied areas of the fast-changing topic of digital control.
Categories: Technology & Engineering

Naval Forces Capability for Theater Missile Defense

Naval Forces  Capability for Theater Missile Defense

... fire control system (manned only to intervene in automatic process); Mk-57, •
Current sea sparrow missile (RIM-7P), based on Navy AIM-7F sparrow air-to-air
missile, • Same booster, guidance, and control with remote arming and “homing
all ...

Author: National Research Council

Publisher: National Academies Press

ISBN: 9780309170963

Category: Technology & Engineering

Page: 204

View: 560

At the request of the Chief of Naval Operations, the National Research Council, under the auspices of the Naval Studies Board, established a committee to assess the Department of the Navy's current and future naval theater missile defense (TMD) capabilities. The Committee for Naval Forces' Capability for Theater Missile Defense first convened in April 2000 and met approximately 2 days a month for 8 months. This report is based on the information presented to the committee during that period and on the committee members' accumulated experience and expertise in military operations, systems, and technologies.
Categories: Technology & Engineering

Miss Distance Analysis in Homing and Lambert Interceptions with Application to a New Guidance Law

Miss Distance Analysis in Homing and Lambert Interceptions with Application to a New Guidance Law

[ 42 ] Gupta , N. K. and Sridhar , B. , Reachable Sets for Missile Guidance against
Smart Targets , IEEE Proceedings of ... [ 49 ] Alpert J. , Miss Distance Analysis for
Command Guided Missiles , Journal of Guidance , Control and Dynamics , Vol.11
 ...

Author: Joon Hyung Park

Publisher:

ISBN: UOM:39015043233165

Category:

Page:

View: 456

Categories:

Journal of Guidance and Control

Journal of Guidance and Control

Stallard , D . V . , " Classical and Modern Guidance of Homing Interceptor
Missiles , ” Missile Systems Div . , Raytheon Co . ... 10 George , L . C . , “ Missile
Guidance and Control System Design Trends , " SAE Paper SAE National
Aerospace ...

Author:

Publisher:

ISBN: UOM:39015013046993

Category: Aeronautics

Page:

View: 224

Categories: Aeronautics

Tactical and Strategic Missile Guidance

Tactical and Strategic Missile Guidance

Linearization of the nonlinear missile - target geometry was shown to be an
accurate approximation to the actual ... Fossier , M . W . , " The Development of
Radar Homing Missiles , ” Journal of Guidance , Control , and Dynamics , Vol . 7 ,
Nov .

Author: Paul Zarchan

Publisher: Amer Inst of Aeronautics &

ISBN: UOM:39015032207238

Category: Science

Page: 452

View: 783

Categories: Science

Optimal Control Theory for Applications

Optimal Control Theory for Applications

Examples of path constraints are control inequality constraints or state inequality
constraints. ... To provide some physical feeling for guidance, consider the case
of a constant speed homing missile attacking a constant velocity target. If the line
 ...

Author: David G. Hull

Publisher: Springer Science & Business Media

ISBN: 0387400702

Category: Technology & Engineering

Page: 384

View: 724

The published material represents the outgrowth of teaching analytical optimization to aerospace engineering graduate students. To make the material available to the widest audience, the prerequisites are limited to calculus and differential equations. It is also a book about the mathematical aspects of optimal control theory. It was developed in an engineering environment from material learned by the author while applying it to the solution of engineering problems. One goal of the book is to help engineering graduate students learn the fundamentals which are needed to apply the methods to engineering problems. The examples are from geometry and elementary dynamical systems so that they can be understood by all engineering students. Another goal of this text is to unify optimization by using the differential of calculus to create the Taylor series expansions needed to derive the optimality conditions of optimal control theory.
Categories: Technology & Engineering