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Missile Dynamics Equations For Guidance And Control Modeling And Analysis
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Book Synopsis Missile Dynamics Equations for Guidance and Control Modeling and Analysis by :
Download or read book Missile Dynamics Equations for Guidance and Control Modeling and Analysis written by and published by . This book was released on 1984 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents some techniques used in deriving the equations of motion of a missile for a six-degree-of-freedom (6-DOF) simulation. Several forms of the equations are developed, and their implementation is discussed. Specific emphasis is placed on showing the interrelation of the equation forms currently in use by showing their development from the basic laws. This report is meant to serve as a primer for new engineers and as a reference for all engineers involved in missile flight simulation.
Book Synopsis Missile Dynamics Equations for Guidance and Control Modeling and Analysis by : Philip N. Jenkins
Download or read book Missile Dynamics Equations for Guidance and Control Modeling and Analysis written by Philip N. Jenkins and published by . This book was released on 1976 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report documents some techniques used in deriving the equations of motion of a missile for a six-degree-of-freedom (6-DOF) simulation. Several forms of the equations are developed, and their implementation is discussed. Specific emphasis is placed on showing the interrelation of the equation forms currently in use by showing their development from the basic laws. This report is meant to serve as a primer for new engineers and as a reference for all engineers involved in missile flight simulation.
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
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 2007-09-20 with total page 242 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 disc
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.
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
Book Synopsis Digital Computer Program for General Missile Dynamics Simulation (n-stage) Summary of Equations by : E. A. Juarez
Download or read book Digital Computer Program for General Missile Dynamics Simulation (n-stage) Summary of Equations written by E. A. Juarez and published by . This book was released on 1961 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents a summary of the mathematical equations contained in the N-STAGE missile simulation program. This program, written for the IBM 7090 digital computer, is designed to be a flexible, high speed computation tool, useful for guidance system analysis, trajectory design, hardware evaluation, or post-flight analysis of any current or proposed missile system. The simulation is generally complete and in most instances accuracy will be limited only by the accuracy of the input data.
Book Synopsis Close Air Support Missile Guidance and Control Study. Volume 2. Three- Degree-of-Freedom Simulation by : J. Mahig
Download or read book Close Air Support Missile Guidance and Control Study. Volume 2. Three- Degree-of-Freedom Simulation written by J. Mahig and published by . This book was released on 1971 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of the report is to describe in detail the equations used and the form required for the input data to a three-degree-of-freedom simulation of a laser guided missile system. The primary purpose of a three-degree-of- freedom simulation is to make possible the study of the characteristics of a given missile system quickly and economically. Since cross-coupling effects influence a missile's performance through the seeker, autopilot, and missile dynamics, any results obtained must be considered as preliminary until justified by a six-degree-of-freedom simulation. Examples of some of the studies which can be usefully made are optimization of the seeker, autopilot gain, and noise sensitivity. The noise sensitivity studies include not only electronic noise but spot motion and signal loss simulation. Once the parameters for a given missile have been entered, it can be used efficiently even on a small computer since the program only requires 17,000 words of core.
Book Synopsis Modeling of the 6DOF Missile Dynamics Using the NED Axes System by :
Download or read book Modeling of the 6DOF Missile Dynamics Using the NED Axes System written by and published by . This book was released on 1997 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: High fidelity and validated six-degree-of-freedom (6DOF) missile simulation models are being developed to accurately model the aerodynamics, guidance, and control characteristics of current tactical air-to-air missiles for system performance assessment. For efficiency, the development of this missile simulation takes advantage of already available model components, such as the modelling of the missile dynamics. However, the documented 6DOF model of missile dynamics currently available is not based on the standard north-east-down (NED) axes system used in most current simulation models. To maintain compatibility with the existing library of components, this missile dynamics model has been modified to use the NED system. This report details those modifications, including information on co-ordinate systems, transformations, equations of motion, tracking loop dynamics, and simulation control.
Book Synopsis Dynamic Modeling, Guidance, and Control of Homing Missiles by :
Download or read book Dynamic Modeling, Guidance, and Control of Homing Missiles written by and published by . This book was released on 2005 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis Missile Flight Simulation by : Jeffrey Strickland
Download or read book Missile Flight Simulation written by Jeffrey Strickland and published by Lulu.com. This book was released on 2015 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt: A missile flight simulation is a computational tool that calculates the flight of a missile from launch until it engages the target. The simulation is based on mathematical models of the missile, target and environment. This book provides instruction for the preparation of these mathematical models to simulate the flight of a surface-to-air missile. The 2nd Edition of Missile Flight Simulation provides updated simulation processes using MATLAB(R) and Simulink(TM), while improving and clarifying previous content. The book may be used as a reference or as a textbook, although it is devoid of exercises. However, the reader is encouraged to perform the simulation of Charter 12 using MATLAB(R) and Simulink(TM), or a programming language such as FORTRAN (see Chapter 10). The book is not intended to be a missile flight engineering reference and does not contain every aspect of missile flight. It provides the appropriate content for simulating missile flight from launch to terminus only.
Book Synopsis Design of Guidance and Control Systems for Tactical Missiles by : Qi Zaikang
Download or read book Design of Guidance and Control Systems for Tactical Missiles written by Qi Zaikang and published by CRC Press. This book was released on 2019-09-09 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design of Guidance and Control Systems for Tactical Missiles presents a modern, comprehensive study of the latest design methods for tactical missile guidance and control. It analyzes autopilot designs, seeker system designs, guidance laws and theories, and the internal and external disturbances affecting the performance factors of missile guidance control systems. The text combines detailed examination of key theories with practical coverage of methods for advanced missile guidance control systems. It is valuable content for professors and graduate-level students in missile guidance and control, as well as engineers and researchers who work in the area of tactical missile guidance and control.
Book Synopsis Body fixed missile analysis by : Gerald Cook
Download or read book Body fixed missile analysis written by Gerald Cook and published by . This book was released on 1981 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mathematical Models for a Missile Autopilot Design by : Farhan A. Faruqi
Download or read book Mathematical Models for a Missile Autopilot Design written by Farhan A. Faruqi and published by . This book was released on 2002 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Book Synopsis Dynamic Equations for Missile Stability Analysis by : J. L. HIEATT
Download or read book Dynamic Equations for Missile Stability Analysis written by J. L. HIEATT and published by . This book was released on 1960 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report develops a method of presenting missile dynamics such that the equations may be easily adapted to any missile system configuration. Standardization of the missile dynamic equations is accomplished by combining the effects of propellant sloshing, flexible vehicle structure, and engine dynamics in a set of orthogonal coordinates. This approach is termed 'combined mode representation'. The theory of combined mode representation is presented in general terms. The complete missile system dynamic equations are then derived using this representation. The derivation of the equations for obtaining the combined mode coordinates is followed by a description of the computer routine used to solve these equations. Finally an example control system problem is written in terms of combined modes. (Author).
Author :Paul Zarchan Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :650 pages Book Rating :4.3/5 (91 download)
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 AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1997 with total page 650 pages. Available in PDF, EPUB and Kindle. Book excerpt: For both experts and novices, presents the principles of both tactical and strategic missile guidance in a common language, notation, and perspective, with numerous examples to illustrate the concepts. This revised edition (1st ed., 1990) adds three new chapters on the fundamentals of endoatmospheric ballistic targets; a new chapter showing how covariance analysis can be used to analyze missile guidance systems; two new appendices; and included Macintosh and IBM compatible formatted disks containing the FORTRAN code listings presented in the text. Annotation copyright by Book News, Inc., Portland, OR
