Optimal Guidance and Its Applications in Missiles and UAVs

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Author :
Publisher : Springer Nature
ISBN 13 : 3030473481
Total Pages : 214 pages
Book Rating : 4.88/5 ( 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

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Publisher : CRC Press
ISBN 13 : 1439850968
Total Pages : 373 pages
Book Rating : 4.61/5 ( 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

Advances in Missile Guidance, Control, and Estimation

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Publisher : CRC Press
ISBN 13 : 1420083147
Total Pages : 720 pages
Book Rating : 4.49/5 ( 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

Missile Guidance and Pursuit

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Author :
Publisher : Elsevier
ISBN 13 : 1782420592
Total Pages : 276 pages
Book Rating : 4.90/5 ( 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

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Author :
Publisher : Springer
ISBN 13 : 3319175181
Total Pages : 740 pages
Book Rating : 4.88/5 ( 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 740 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

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Publisher : Springer Science & Business Media
ISBN 13 : 0387218165
Total Pages : 670 pages
Book Rating : 4.68/5 ( 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

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Publisher : Springer
ISBN 13 : 3319652834
Total Pages : 751 pages
Book Rating : 4.32/5 ( 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 751 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.

Modern Missile Guidance

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Publisher : CRC Press
ISBN 13 : 1351202936
Total Pages : 335 pages
Book Rating : 4.30/5 ( 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 335 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.

State Estimation and Control for Low-cost Unmanned Aerial Vehicles

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Publisher : Springer
ISBN 13 : 3319164171
Total Pages : 232 pages
Book Rating : 4.75/5 ( download)

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Book Synopsis State Estimation and Control for Low-cost Unmanned Aerial Vehicles by : Chingiz Hajiyev

Download or read book State Estimation and Control for Low-cost Unmanned Aerial Vehicles written by Chingiz Hajiyev and published by Springer. This book was released on 2015-06-10 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book discusses state estimation and control procedures for a low-cost unmanned aerial vehicle (UAV). The authors consider the use of robust adaptive Kalman filter algorithms and demonstrate their advantages over the optimal Kalman filter in the context of the difficult and varied environments in which UAVs may be employed. Fault detection and isolation (FDI) and data fusion for UAV air-data systems are also investigated, and control algorithms, including the classical, optimal, and fuzzy controllers, are given for the UAV. The performance of different control methods is investigated and the results compared. State Estimation and Control of Low-Cost Unmanned Aerial Vehicles covers all the important issues for designing a guidance, navigation and control (GNC) system of a low-cost UAV. It proposes significant new approaches that can be exploited by GNC system designers in the future and also reviews the current literature. The state estimation, control and FDI methods are illustrated by examples and MATLAB® simulations. State Estimation and Control of Low-Cost Unmanned Aerial Vehicles will be of interest to both researchers in academia and professional engineers in the aerospace industry. Graduate students may also find it useful, and some sections are suitable for an undergraduate readership.

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

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Publisher :
ISBN 13 : 9781423533528
Total Pages : 222 pages
Book Rating : 4.26/5 ( 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.