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Design of Guidance & Control Systems for Tactical Missiles
Original price was: ₹11,954.70.₹9,563.76Current price is: ₹9,563.76.
ISBN: 9780367260415
Author/Editor: Qi Zaikang
Publisher: CRC Press
Year: 2020
Available on backorder
Description
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.
Additional information
Weight | 0.65 kg |
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Product Properties
Year of Publication | 2020 |
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Table of Contents | Table of Contents 1. The Basics of Missile Guidance Control 1.1. Overview 1.2. Missile Control Methods 2. Missile Trajectory Models, Aerodynamic Derivatives, Dynamic Coefficients and Missile Transfer Functions 2.1 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 Models 3.1 Seeker 3.2 Actuator 3.3 Angular Rate Gyro 3.4 Accelerometer 3.5 Inertial Navigation Components and Integrated Inertial Navigation Module 4. Autopilot Design 4.1 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 radar 5.1 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 Guidance Radar 5.5 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 Guidance 6.1 LOS Guidance System 6.2 Analysis of the Required Acceleration for the Missile with LOS Guidance 6.3 Analysis of the LOS Guidance Loop 6.4 Lead Angle Method 7. Seekers 7.1 Overview 7.2 Electromechanical Structure of Commonly Used Seekers 7.3 Mechanism Analysis of the Anti-disturbance Moment of the Seeker's Stabilization Loop and Tracking Loop 7.4 Transfer Function of Body Motion Coupling and Parasitic Loop 7.5 A Real Seeker Model 7.6 Other Parasitic Loop Models 7.7 Stabilization Loop and Tracking Loop Design of the Platform Based Seeker 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 Laws 8.4 Target Maneuver Acceleration Estimation 8.5 Optimum Trajectory Control Design Appendix. I Proof of the Proportional Navigation Law with the Help of Optimal Control Theory Appendix. II Adjoint Method Bibliography Index |
Author | Qi Zaikang |
ISBN/ISSN | 9780367260415 |
Binding | Hardback |
Edition | 1 |
Publisher | CRC Press |
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