Principles of Modern Radar Missile Seekers.

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Place / Publishing House:Norwood : : Artech House,, 2022.
Ã2022.
Year of Publication:2022
Edition:1st ed.
Language:English
Online Access:
Physical Description:1 online resource (443 pages)
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Table of Contents:
  • Intro
  • Principles of Modern Radar Missile Seekers
  • Contents
  • Preface
  • Acknowledgments
  • CHAPTER 1 Introduction
  • 1.1 Threats
  • 1.1.1 The First Threat
  • 1.1.2 The Second Threat
  • 1.1.3 The Third Threat
  • 1.2 Goals and Objectives
  • 1.3 Basic Concepts
  • References
  • CHAPTER 2 Tactical and Technical Characteristics of an Anti-Aircraft Missile System
  • 2.1 The Defeat Zone
  • 2.1.1 Choosing the Anti-Aircraft Missile System Defeat Zone Boundaries
  • 2.1.2 Providing a Given Defeat Zone with the Technical Characteristics of Anti-Aircraft Missile System Combat Requirements
  • 2.2 Missile Launch Zone
  • 2.3 A Target Detection Zone
  • References
  • CHAPTER 3 Firing over the Horizon
  • 3.1 Basic Principles
  • 3.2 Estimate of Ballistic and Flight Characteristics of the Missile According to Data From Open Sources
  • 3.3 Problems: Target Search and Auto-Tracking
  • References
  • CHAPTER 4 Radio Control of Atmospheric Anti-Aircraft Missile
  • 4.1 Generalized Block Diagram of the Radio System
  • 4.2 Radio Control System Classification
  • 4.2.1 Launch Control
  • 4.2.2 Anti-Aircraft Missile Flight Control
  • 4.2.3 Missile Warhead Detonation Control
  • 4.3 Flight Trajectories and Guidance Methods
  • 4.3.1 Two-Point Guidance Methods: Homing Methods
  • 4.3.2 Three-Point Guidance Methods: Teleguidance Methods
  • References
  • CHAPTER 5 Radar
  • 5.1 Basic Principles
  • 5.2 Radar Types
  • 5.2.1 Search and Detect Radars
  • 5.2.2 Tracking Radars
  • 5.2.3 Image Radars
  • 5.3 Tactical and Technical Characteristics of the Radar
  • References
  • CHAPTER 6 Monopulse Radars
  • 6.1 Basic Principles
  • 6.2 Tracking Radars
  • 6.2.1 Amplitude Sum-and-Difference System of Automatic Target Tracking
  • 6.2.2 Phase Sum-and-Difference System of Automatic Target Tracking
  • 6.3 Monopulse Antenna
  • 6.3.1 Lens Antennas
  • 6.3.2 Reflector Antennas
  • 6.3.3 Arrays Antennas.
  • 6.4 Cross-Polarization Radiation
  • 6.5 Radar Resolution on Angular Coordinates
  • References
  • CHAPTER 7 Some Interferences for Monopulse Radar
  • 7.1 Camouflaging Interference
  • 7.1.1 Active Camouflaging Interference
  • 7.1.2 Passive Camouflaging Interference
  • 7.2 Active Misinforming Interference
  • 7.3 Interference due to High-Altitude Nuclear Explosions:Electromagnetic Weapons
  • References
  • CHAPTER 8 Interference Immunity of Monopulse Radar
  • 8.1 Interference Immunity Indicators
  • 8.2 Criterion for Assessing the Stability of Automatic Target Tracking by Monopulse Radar in Real Time
  • References
  • CHAPTER 9 Modeling
  • 9.1 Formation Procedure of the Direction-Finding Characteristic
  • 9.2 The Initial Impacts Classification
  • 9.3 Formation Method of Stochastic Orthogonal Processes
  • References
  • CHAPTER 10 Interference Detection Problem
  • 10.1 Testing a Simple Hypothesis Against a Simple Alternative
  • 10.2 Testing a Complex Hypothesis Against a Simple Alternative
  • 10.3 Determination of Estimates of the Maximum Similarities
  • 10.4 Interference Recognition Procedure
  • 10.4.1 Estimation of the Required Range of a Hypersonic Target Detection by the Missile Homing Head when Firing over the Horizon
  • 10.4.2 Recognition Procedure for Some Interference Types
  • References
  • CHAPTER 11 Assessment of an Anti-Aircraft Missile System Operation in Interference Conditions
  • 11.1 Assessment Probability of Target Defeat by One Missile
  • 11.2 Radomes and Estimation of the Active Seeker Operating Wavelength
  • 11.3 Operation of an Active Homing Head on a Group of Targets-Self-Cover Jammers
  • 11.4 Probability a Target is Defeated by One Missile
  • 11.5 Operating Principles of a Modern Anti-Aircraft Missile System on a Group Target
  • 11.5.1 The Work of an Active Homing Head on a Group of Targets: Self-Cover Jammers.
  • 11.6 Operation of the Active Homing Head When Auto-Tracking a Low-Attitude Clean Target and Using an Antipode Jammer
  • 11.6.1 Signal Processing and Decision Rules
  • 11.6.2 Operation of the Active Seeker on the Clean Target, Which Creates a Mirror Image from the Earth's (Water's) Surface
  • 11.6.3 The Work of the Active Seeker on a Target, that Creates Interference such as Antipode
  • References
  • CHAPTER 12 Synthesis of Solutions on Improving Interference Immunity Against the Impact of Polarization Interference
  • 12.1 Calculation of Direction-Finding Characteristics
  • 12.2 Assessing Accuracy of an Angular Auto-Tracking System of the Target under Conditions of Polarization Interfe
  • 12.3 Stability of Target Auto-Tracking in Conditions of Polarization Interference
  • 12.4 The Decision Synthesis, Providing Auto-Tracking Stability of the Polarization Interference Source
  • 12.5 Evaluation of the Stability of an Angular Auto-Tracking System of a Target Under Conditions of Polarization Interference
  • 12.6 Proposals to Improve the Interference Immunity of a Monopulse Direction Finder to the Effects of Polarization Interference
  • 12.6.1 Operation of Prototype Mode: 1A
  • 12.6.2 Operation in Mode of the Proposed Decision: 1B
  • 12.6.3 Operation of Prototype Mode: 2A
  • 12.6.4 Operation in Mode of the Proposed Decision: 2B
  • 12.7 The Interference Immunity Indicator
  • 12.8 Conclusion
  • References
  • CHAPTER 13 Solutions Synthesis to Increase the Noise Immunity of an Active Homing Head
  • 13.1 Interference Immunity of a Missile Homing Head from Interference Along the Sidelobes of its Directional Pattern
  • 13.2 Operation Assessment of the Air Defense Missile System for High-Speed and Low-Altitude Targets Without Interferen
  • 13.2.1 Methods for Overcoming the Defeat Zone of an Anti-Aircraft Missile System.
  • 13.3 Solution Synthesis to Increase the Interference Immunity of an Active Homing Head During its Operation at Low-Altitude Targets and by a Group of Jammers
  • 13.3.1 Options Analysis for Increasing the Accuracy and Formulation of the Synthesis Problem
  • 13.3.2 Solution Synthesis
  • 13.3.3 Solution for the Emitted Signal, Taking into Account the Limitations due to the Hardware Implementation of the Anti-Aircraft Missile System
  • 13.3.4 Proposals for the Hardware Implementation of a Synthesized Solution in a Real Anti-Aircraft Missile System
  • References
  • CHAPTER 14 Determining Performance Limitationsof Existing Air Defense Systems for Intercepting Hypersonic Vehicles
  • 14.1 Introduction
  • 14.2 Field Scatter Pattern Calculation Mathematics
  • 14.3 Evaluation of Interception Hypersonic Vehicles by Some Existing Air Defense Missile Systems
  • 14.4 Calculation Results
  • 14.5 Conclusion
  • References
  • Acronyms and Abbreviations
  • About the Author
  • Index.