Design of guidance and control systems for tactical missiles / (Record no. 129352)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 04955cam a2200553Ki 4500 |
| 001 - CONTROL NUMBER | |
| control field | 9780429291203 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | FlBoTFG |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220509193057.0 |
| 006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS--GENERAL INFORMATION | |
| fixed length control field | m o d |
| 007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION | |
| fixed length control field | cr cnu|||unuuu |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 190912s2020 flu o 000 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Original cataloging agency | OCoLC-P |
| Language of cataloging | eng |
| Description conventions | rda |
| -- | pn |
| Transcribing agency | OCoLC-P |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9780429291203 |
| -- | (electronic bk.) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 0429291205 |
| -- | (electronic bk.) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9781000681215 |
| -- | (electronic bk. : EPUB) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 1000681211 |
| -- | (electronic bk. : EPUB) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9781000680676 |
| -- | (electronic bk. : PDF) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 1000680673 |
| -- | (electronic bk. : PDF) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9781000680942 |
| -- | (electronic bk. : Mobipocket) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 1000680940 |
| -- | (electronic bk. : Mobipocket) |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| Cancelled/invalid ISBN | 9780367260415 |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| Cancelled/invalid ISBN | 0367260417 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (OCoLC)1119391281 |
| Canceled/invalid control number | (OCoLC)1119535208 |
| 035 ## - SYSTEM CONTROL NUMBER | |
| System control number | (OCoLC-P)1119391281 |
| 050 #4 - LIBRARY OF CONGRESS CALL NUMBER | |
| Classification number | TL589.4 |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TEC |
| Subject category code subdivision | 007000 |
| Source | bisacsh |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TEC |
| Subject category code subdivision | 009020 |
| Source | bisacsh |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TEC |
| Subject category code subdivision | 009070 |
| Source | bisacsh |
| 072 #7 - SUBJECT CATEGORY CODE | |
| Subject category code | TQ |
| Source | bicssc |
| 082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.1326 |
| Edition number | 23 |
| 100 1# - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Zaikang, Qi, |
| Relator term | author. |
| 245 10 - TITLE STATEMENT | |
| Title | Design of guidance and control systems for tactical missiles / |
| Statement of responsibility, etc | Qi Zaikang and Lin Defu. |
| 250 ## - EDITION STATEMENT | |
| Edition statement | First edition. |
| 264 #1 - | |
| -- | Boca Raton : |
| -- | CRC Press, |
| -- | 2020. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 1 online resource (xiv, 240 pages). |
| 336 ## - | |
| -- | text |
| -- | txt |
| -- | rdacontent |
| 337 ## - | |
| -- | computer |
| -- | c |
| -- | rdamedia |
| 338 ## - | |
| -- | online resource |
| -- | cr |
| -- | rdacarrier |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Formatted contents note | Table of Contents1. The Basics of Missile Guidance Control1.1. Overview1.2. Missile Control Methods 2. Missile Trajectory Models, Aerodynamic Derivatives, Dynamic Coefficients and Missile Transfer Functions2.1 Symbols and Definitions 2.2 Euler Equations of the Missile Rigid Body Motion 2.3 Configuration of the Control Surfaces 2.4 Aerodynamic Derivatives and the Missile Control Dynamic Coefficient 2.5 The Transfer Function of a Missile the Object Being Controlled 3. Basic Missile Control Component Mathematics Models3.1 Seeker 3.2 Actuator 3.3 Angular Rate Gyro 3.4 Accelerometer 3.5 Inertial Navigation Components and Integrated Inertial Navigation Module 4. Autopilot Design4.1 Acceleration Autopilot 4.2 Pitch/Yaw Attitude Autopilot 4.3 Flight Path Angle Autopilot 4.4 Roll Attitude Autopilot 4.5 BTT Autopilot 4.6 Thrust vector control and thruster control 5. Guidance radar5.1 Introduction 5.2 Motion Characteristic of the Target Line-of-Sight 5.3 Loop of the Guidance Radar Control 5.4 Effect of the Receiver Thermal Noise on the Performance of GuidanceRadar5.5 Effect of Target Glint on the Performance of Guidance Radar 5.6 Effect of Other Disturbances on the Performance of Guidance Radar 6. Line of Sight Guidance6.1 LOS Guidance System6.2 Analysis of the Required Acceleration for the Missile with LOSGuidance6.3 Analysis of the LOS Guidance Loop6.4 Lead Angle Method 7. Seekers7.1 Overview7.2 Electromechanical Structure of Commonly Used Seekers7.3 Mechanism Analysis of the Anti-disturbance Moment of the Seeker'sStabilization Loop and Tracking Loop 7.4 Transfer Function of Body Motion Coupling and Parasitic Loop7.5 A Real Seeker Model 7.6 Other Parasitic Loop Models 7.7 Stabilization Loop and Tracking Loop Design of the Platform BasedSeeker 8. Proportional Navigation and Extended Proportional Navigation Guidance Laws 8.1 Proportional Navigation Guidance Law 8.2 Extended Proportional Navigation Guidance Laws (Optimal Proportional Navigation, OPN) 8.3 Other Types of Proportional Navigation Laws8.4 Target Maneuver Acceleration Estimation8.5 Optimum Trajectory Control DesignAppendix. I Proof of the Proportional Navigation Law with the Help of Optimal Control TheoryAppendix. II Adjoint MethodBibliographyIndex |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | Design of Guidanceand 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. |
| 588 ## - | |
| -- | OCLC-licensed vendor bibliographic record. |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | TECHNOLOGY / Electricity |
| Source of heading or term | bisacsh |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | TECHNOLOGY / Engineering / Civil |
| Source of heading or term | bisacsh |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | TECHNOLOGY / Engineering / Mechanical |
| Source of heading or term | bisacsh |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Guided missiles |
| General subdivision | Control systems. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Guided missiles |
| General subdivision | Guidance systems. |
| 700 1# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Defu, Lin, |
| Relator term | author. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Materials specified | Taylor & Francis |
| Uniform Resource Identifier | https://www.taylorfrancis.com/books/9780429291203 |
| 856 42 - ELECTRONIC LOCATION AND ACCESS | |
| Materials specified | OCLC metadata license agreement |
| Uniform Resource Identifier | http://www.oclc.org/content/dam/oclc/forms/terms/vbrl-201703.pdf |
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