Optimal Guidance And Its Applications In Missiles And Uavs

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Optimal Guidance and Its Applications in Missiles and UAVs

Author : Shaoming He
Publisher : Springer Nature
ISBN 13 : 3030473481
Total Pages : 214 pages
Book Rating : 4.0/5 (34 download)

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Book Synopsis Optimal Guidance and Its Applications in Missiles and UAVs by : Shaoming He

Download or read book Optimal Guidance and Its Applications in Missiles and UAVs written by Shaoming He and published by Springer Nature. This book was released on 2020-05-13 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents a comprehensive overview of the recent advances in the domain of optimal guidance, exploring the characteristics of various optimal guidance algorithms and their pros and cons. Optimal guidance is based on the concept of trajectory optimization, which minimizes the meaningful performance index while satisfying certain terminal constraints, and by properly designing the cost function the guidance command can serve as a desired pattern for a variety of mission objectives. The book allows readers to gain a deeper understanding of how optimal guidance law can be utilized to achieve different mission objectives for missiles and UAVs, and also explores the physical meaning and working principle of different new optimal guidance laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority.

Guidance of Unmanned Aerial Vehicles

Author : Rafael Yanushevsky
Publisher : CRC Press
ISBN 13 : 9781439850954
Total Pages : 376 pages
Book Rating : 4.8/5 (59 download)

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Book Synopsis Guidance of Unmanned Aerial Vehicles by : Rafael Yanushevsky

Download or read book Guidance of Unmanned Aerial Vehicles written by Rafael Yanushevsky and published by CRC Press. This book was released on 2011-03-29 with total page 376 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written by an expert with more than 30 years of experience, Guidance of Unmanned Aerial Vehicles contains new analytical results, taken from the author’s research, which can be used for analysis and design of unmanned aerial vehicles guidance and control systems. This book progresses from a clear elucidation of guidance laws and unmanned aerial vehicle dynamics to the modeling of their guidance and control systems. Special attention is paid to guidance of autonomous UAVs, which differs from traditional missile guidance. The author explains UAV applications, contrasting them to a missile’s limited ability (or inability) to control axial acceleration. The discussion of guidance laws for UAVs presents a generalization of missile guidance laws developed by the author. The computational algorithms behind these laws are tested in three applications—for the surveillance problem, the refueling problem, and for the motion control of a swarm of UAVs. The procedure of choosing and testing the guidance laws is also considered in an example of future generation of airborne interceptors launched from UAVs. The author provides an innovative presentation of the theoretical aspects of unmanned aerial vehicles’ guidance that cannot be found in any other book. It presents new ideas that, once crystallized, can be implemented in the new generation of unmanned aerial systems.

Missile Guidance and Pursuit

Author : N A Shneydor
Publisher : Elsevier
ISBN 13 : 1782420592
Total Pages : 276 pages
Book Rating : 4.7/5 (824 download)

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Book Synopsis Missile Guidance and Pursuit by : N A Shneydor

Download or read book Missile Guidance and Pursuit written by N A Shneydor and published by Elsevier. This book was released on 1998-01-01 with total page 276 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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

Advances in Aerospace Guidance, Navigation and Control

Author : Joël Bordeneuve-Guibé
Publisher : Springer
ISBN 13 : 3319175181
Total Pages : 730 pages
Book Rating : 4.3/5 (191 download)

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Book Synopsis Advances in Aerospace Guidance, Navigation and Control by : Joël Bordeneuve-Guibé

Download or read book Advances in Aerospace Guidance, Navigation and Control written by Joël Bordeneuve-Guibé and published by Springer. This book was released on 2015-04-04 with total page 730 pages. Available in PDF, EPUB and Kindle. Book excerpt: The two first CEAS (Council of European Aerospace Societies) Specialist Conferences on Guidance, Navigation and Control (CEAS EuroGNC) were held in Munich, Germany in 2011 and in Delft, The Netherlands in 2013. ONERA The French Aerospace Lab, ISAE (Institut Supérieur de l’Aéronautique et de l’Espace) and ENAC (Ecole Nationale de l’Aviation Civile) accepted the challenge of jointly organizing the 3rd edition. The conference aims at promoting new advances in aerospace GNC theory and technologies for enhancing safety, survivability, efficiency, performance, autonomy and intelligence of aerospace systems. It represents a unique forum for communication and information exchange between specialists in the fields of GNC systems design and operation, including air traffic management. This book contains the forty best papers and gives an interesting snapshot of the latest advances over the following topics: l Control theory, analysis, and design l Novel navigation, estimation, and tracking methods l Aircraft, spacecraft, missile and UAV guidance, navigation, and control l Flight testing and experimental results l Intelligent control in aerospace applications l Aerospace robotics and unmanned/autonomous systems l Sensor systems for guidance, navigation and control l Guidance, navigation, and control concepts in air traffic control systems For the 3rd CEAS Specialist Conference on Guidance, Navigation and Control the International Program Committee conducted a formal review process. Each paper was reviewed in compliance with standard journal practice by at least two independent and anonymous reviewers. The papers published in this book were selected from the conference proceedings based on the results and recommendations from the reviewers.

Missile Guidance and Control Systems

Author : George M. Siouris
Publisher : Springer Science & Business Media
ISBN 13 : 0387218165
Total Pages : 670 pages
Book Rating : 4.3/5 (872 download)

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Book Synopsis Missile Guidance and Control Systems by : George M. Siouris

Download or read book Missile Guidance and Control Systems written by George M. Siouris and published by Springer Science & Business Media. This book was released on 2006-05-07 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Advances in Aerospace Guidance, Navigation and Control

Author : Bogusław Dołęga
Publisher : Springer
ISBN 13 : 3319652834
Total Pages : 735 pages
Book Rating : 4.3/5 (196 download)

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Book Synopsis Advances in Aerospace Guidance, Navigation and Control by : Bogusław Dołęga

Download or read book Advances in Aerospace Guidance, Navigation and Control written by Bogusław Dołęga and published by Springer. This book was released on 2017-12-15 with total page 735 pages. Available in PDF, EPUB and Kindle. Book excerpt: The first three CEAS (Counsil of European Aerospace Societies) Specialist Conferences on Guidance, Navigation and Control (CEAS EuroGNC) were held in Munich, Germany in 2011, in Delft, Netherlands in 2013 and in Toulouse, France in 2017. The Warsaw University of Technology (WUT) and the Rzeszow University of Technology (RzUT) accepted the challenge of jointly organizing the 4th edition. The conference aims to promote scientific and technical excellence in the fields of Guidance, Navigation and Control (GNC) in aerospace and other fields of technology. The Conference joins together the industry with the academia research. This book covers four main topics: Guidance and Control, Control Theory Application, Navigation, UAV Control and Dynamic. The papers included focus on the most advanced and actual topics in guidance, navigation and control research areas: · Control theory, analysis, and design · ; Novel navigation, estimation, and tracking methods · Aircraft, spacecraft, missile and UAV guidance, navigation, and control · Flight testing and experimental results · Intelligent control in aerospace applications · Aerospace robotics and unmanned/autonomous systems · Sensor systems for guidance, navigation and control · Guidance, navigation, and control concepts in air traffic control systems For the 4th CEAS Specialist Conference on Guidance, Navigation and Control the International Technical Committee established a formal review process. Each paper was reviewed in compliance with good journal practices by independent and anonymous reviewers. At the end of the review process papers were selected for publication in this book.

Basics of Missile Guidance and Space Techniques

Author : Marvin Hobbs
Publisher : Wildside Press LLC
ISBN 13 : 1434421252
Total Pages : 156 pages
Book Rating : 4.4/5 (344 download)

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Book Synopsis Basics of Missile Guidance and Space Techniques by : Marvin Hobbs

Download or read book Basics of Missile Guidance and Space Techniques written by Marvin Hobbs and published by Wildside Press LLC. This book was released on 2010-06-01 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Tactical and Strategic Missile Guidance

Author : Paul Zarchan
Publisher :
ISBN 13 :
Total Pages : 368 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Tactical and Strategic Missile Guidance by : Paul Zarchan

Download or read book Tactical and Strategic Missile Guidance written by Paul Zarchan and published by . This book was released on 1990 with total page 368 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Advances in Aerospace Guidance, Navigation and Control

Author : Florian Holzapfel
Publisher : Springer Science & Business Media
ISBN 13 : 3642198171
Total Pages : 465 pages
Book Rating : 4.6/5 (421 download)

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Book Synopsis Advances in Aerospace Guidance, Navigation and Control by : Florian Holzapfel

Download or read book Advances in Aerospace Guidance, Navigation and Control written by Florian Holzapfel and published by Springer Science & Business Media. This book was released on 2011-03-15 with total page 465 pages. Available in PDF, EPUB and Kindle. Book excerpt: Over the last few decades, both the aeronautics and space disciplines have greatly influenced advances in controls, sensors, data fusion and navigation. Many of those achievements that made the word “aerospace” synonymous with “high–tech” were enabled by innovations in guidance, navigation and control. Europe has seen a strong trans-national consolidation process in aerospace over the last few decades. Most of the visible products, like commercial aircraft, fighters, helicopters, satellites, launchers or missiles, are not made by a single country – they are the fruits of cooperation. No European country by itself hosts a specialized guidance, navigation and controls community large enough to cover the whole spectrum of disciplines. However, on a European scale, mutual exchange of ideas, concepts and solutions is enriching for all. The 1st CEAS Specialist Conference on Guidance, Navigation and Control is an attempt to bring this community together. This book is a selection of papers presented at the conference. All submitted papers have gone through a formal review process in compliance with good journal practices. The best papers have been recommended by the reviewers to be published in this book.

A Method of Increasing the Kinematic Boundary of Air-to-Air Missiles Using an Optimal Control Approach

Author : Robert D. Broadston
Publisher :
ISBN 13 : 9781423533528
Total Pages : 222 pages
Book Rating : 4.5/5 (335 download)

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Book Synopsis A Method of Increasing the Kinematic Boundary of Air-to-Air Missiles Using an Optimal Control Approach by : Robert D. Broadston

Download or read book A Method of Increasing the Kinematic Boundary of Air-to-Air Missiles Using an Optimal Control Approach written by Robert D. Broadston and published by . This book was released on 2000-09-01 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: Current missile guidance laws are generally based on one of several forms of proportional navigation (PN). While PN laws are robust, analytically tractable, and computationally simple, they are only optimal in a narrow operating regime. Consequently, they may not optimize engagement range, time to intercept, or endgame kinetic energy. The advent of miniaturized high speed computers has made it possible to compute optimal trajectories for missiles using command mid-course guidance as well as autonomous onboard guidance. This thesis employs a simplified six degree of freedom (6DOF) flight model and a full aerodynamic 6DOF flight model to analyze the performance of both PN and optimal guidance laws in a realistic simulation environment which accounts for the effects of drag and control system time constants on the missile's performance. Analysis of the missile's kinematic boundary is used as the basis of comparison. A missile's kinematic boundary can be described as the maximum theoretical range at which it can intercept a target assuming no noise in its sensors. This analysis is immediately recognizable to the warfighter as an engagement envelope. The guidance laws are tested against non-maneuvering and maneuvering aircraft targets and against a simulation of a cruise missile threat. An application of the 6DOF model for a theater ballistic missile interceptor is presented.

Modern Missile Guidance

Author : Rafael Yanushevsky
Publisher : CRC Press
ISBN 13 : 1351202936
Total Pages : 372 pages
Book Rating : 4.3/5 (512 download)

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Book Synopsis Modern Missile Guidance by : Rafael Yanushevsky

Download or read book Modern Missile Guidance written by Rafael Yanushevsky and published by CRC Press. This book was released on 2018-09-17 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt: Missile Guidance, Second Edition provides a timely survey of missile control and guidance theory, based on extensive work the author has done using the Lyapunov approach. This new edition also presents the Lyapunov-Bellman approach for choosing optimal parameters of the guidance laws, and direct and inverse optimal problems are considered. This material is important for readers working in the areas of optimization and optimal theory. This edition also contains updated coverage of guidance and control system components, since the efficiency of guidance laws depends on their realization. The text concludes with information on the new generation of intercept systems now in development.

Guidance of Unmanned Aerial Vehicles

Author : Rafael Yanushevsky
Publisher : CRC Press
ISBN 13 : 1439850968
Total Pages : 373 pages
Book Rating : 4.4/5 (398 download)

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Book Synopsis Guidance of Unmanned Aerial Vehicles by : Rafael Yanushevsky

Download or read book Guidance of Unmanned Aerial Vehicles written by Rafael Yanushevsky and published by CRC Press. This book was released on 2011-03-29 with total page 373 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written by an expert with more than 30 years of experience, Guidance of Unmanned Aerial Vehicles contains new analytical results, taken from the author's research, which can be used for analysis and design of unmanned aerial vehicles guidance and control systems. This book progresses from a clear elucidation of guidance laws and unmanned aerial veh

A New Paradigm in Optimal Missile Guidance

Author : Robert W. Morgan
Publisher :
ISBN 13 :
Total Pages : 770 pages
Book Rating : 4.:/5 (659 download)

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Book Synopsis A New Paradigm in Optimal Missile Guidance by : Robert W. Morgan

Download or read book A New Paradigm in Optimal Missile Guidance written by Robert W. Morgan and published by . This book was released on 2007 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt: This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of missile guidance usually lasts less than ten seconds and calls for very accurate maneuvering to ensure intercept. Technological advancements have produced increasingly sophisticated threats that greatly reduce the effectiveness of traditional approaches to missile guidance. Because of this, terminal missile guidance is, and will remain, an important and active area of research. The complexity of the problem and the desire for an optimal solution has resulted in researchers focusing on simplistic, usually linear, models. The fruit of these endeavors has resulted in some of the world's most advanced weapons systems. Even so, the resulting guidance schemes cannot possibly counter the evolving threats that will push the system outside the linear envelope for which they were designed. The research done in this dissertation greatly extends previous research in the area of optimal missile guidance. Herein it is shown that optimal missile guidance is fundamentally a pairing of an optimal guidance strategy and an optimal control strategy. The optimal guidance strategy is determined from a missile's information constraints, which are themselves largely determined from the missile's sensors. The optimal control strategy is determined by the missile's control constraints, and works to achieve a specified guidance strategy. This dichotomy of missile guidance is demonstrated by showing that missiles having different control constraints utilize the same guidance strategy so long as the information constraints are the same. This concept has hitherto been unrecognized because of the difficulty in developing an optimal control for the nonlinear set of equations that result from control constraints. Having overcome this difficulty by indirect means, evidence of the guidance strategy paradigm emerged. The guidance strategy paradigm is used to develop two advanced guidance laws. The new guidance laws are compared qualitatively and quantitatively with existing guidance laws.

Optimal Guidance Anticipating Missile Performance

Author : W. Grimm
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (228 download)

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Book Synopsis Optimal Guidance Anticipating Missile Performance by : W. Grimm

Download or read book Optimal Guidance Anticipating Missile Performance written by W. Grimm and published by . This book was released on 1992 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two different guidance methods are designed for the pre-launch phase in a one-versus-one air combat situation with missiles. In both guidance schemes a missile/target simulation is performed to estimate the miss distance at the end of a fictitious missile launch. A way to do this in real time is described. The first guidance method continuously evaluates the miss distance for each aircraft against the respective opponent. The guidance is such that the ratio of the rates of the miss distances takes an optimal value from the view of the guided aircraft. Thus, it reaches a firing opportunity first.

Advances in Missile Guidance, Control, and Estimation

Author : S.N. Balakrishnan
Publisher : CRC Press
ISBN 13 : 1420083147
Total Pages : 720 pages
Book Rating : 4.4/5 (2 download)

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Book Synopsis Advances in Missile Guidance, Control, and Estimation by : S.N. Balakrishnan

Download or read book Advances in Missile Guidance, Control, and Estimation written by S.N. Balakrishnan and published by CRC Press. This book was released on 2016-04-19 with total page 720 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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

Modern Navigation, Guidance, and Control Processing

Author : Ching-Fang Lin
Publisher :
ISBN 13 :
Total Pages : 712 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Modern Navigation, Guidance, and Control Processing by : Ching-Fang Lin

Download or read book Modern Navigation, Guidance, and Control Processing written by Ching-Fang Lin and published by . This book was released on 1991 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: M->CREATED

Study on Cooperative Missile Guidance for Area Air Defence

Author : H-S. Shin
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (784 download)

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Book Synopsis Study on Cooperative Missile Guidance for Area Air Defence by : H-S. Shin

Download or read book Study on Cooperative Missile Guidance for Area Air Defence written by H-S. Shin and published by . This book was released on 2012 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: This research investigates the necessary components to design cooperative guidance strategies for area air defense applications, as a part of a project supportedby UK MoD and French DGA MCM-ITP (Materials and Components for Missile - Innovation and Technology Partnership) programme. The main considerations in developing the cooperative guidance scheme are the uncertainty of the target manoeuvre and the zone defence concept. For the interception of unpredictable targets before they reach any asset in the defended area, Earliest Intercept Geometry (EIG) and Intercept Geometry (IG) are introduced; EIG is analytically obtained and IG is numerically computed in consideration of physical constraints of the missile and target. Then, two mid course guidance laws are proposed using the geometries, termed the Earliest Intercept Geometry Guidance Law (EIGGL) and Intercept Geometry Guidance Law (IGGL). Since the EIG or IG represents a capture zone of the missile, the defended assets can be protected if the guidance law guarantees no overlapping between the geometry (EIG or IG) and the defended area. In many-on-many engagement scenarios, it is clear that the performance of the guidance scheme depends on the target allocation policy, thus an optimal target allocation algorithm is designed using the EIG and IG to maximize the reachability and safety margin. Multiple co-existing hypotheses about future target trajectory in the mid course and homing phase result in an initial angular difference between actual flight path and the flight path demanded by the homing guidance law at handover, termed the heading error. Even if a hypothesis of future target trajectory is common to mid course and homing guidance laws, heading error can be caused by errors in uplink data because of radar/launcher misalignment, tracker lag, radar measurement error etc. Since this error might result in an abrupt change of the missile acceleration, it is undesirable. In order to resolve this problem, an optimal homing guidance law is developed by introducing a second order polynomial function into the cost function of the guidance problem. The performance of the optimal guidance law heavily depends on the accuracy of the time-to-go estimates. Because the optimal guidance laws are used in the calculation of the IG and the terminal homing guidance, a time-to go estimation algorithm is also proposed. The performance of each algorithm is demonstrated using simple numerical examples. Furthermore, the overall performance of the cooperative guidance algorithm is verified using scenarios in naval and ground context and a Simulink Common Model (CM). For the algorithm test and development, these scenarios and CM have been shared between partners and have evolved during the project. Future work within this research area is discussed further in the last chapter of this thesis, along with other applications for the cooperative guidance scheme.