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A comprehensive resource that explores electromagnetic compatibility (EMC) for aerospace systems
Handbook of Aerospace Electromagnetic Compatibility is a groundbreaking book on EMC for aerospace systems that addresses both aircraft and space vehicles. With contributions from an international panel of aerospace EMC experts, this important text deals with the testing of spacecraft components and subsystems, analysis of crosstalk and field coupling, aircraft communication systems, and much more. The text also includes information on lightning effects and testing, as well as guidance on design principles and techniques for lightning protection.
The book offers an introduction to E³ models and techniques in aerospace systems and explores EMP effects on and technology for aerospace systems. Filled with the most up-to-date information, illustrative examples, descriptive figures, and helpful scenarios, Handbook of Aerospace Electromagnetic Compatibility is designed to be a practical information source. This vital guide to electromagnetic compatibility:
* Provides information on a range of topics including grounding, coupling, test procedures, standards, and requirements
* Offers discussions on standards for aerospace applications
* Addresses aerospace EMC through the use of testing and theoretical approaches
Written for EMC engineers and practitioners, Handbook of Aerospace Electromagnetic Compatibility is a critical text for understanding EMC for aerospace systems.
Inhaltsverzeichnis
Preface ix
Acknowledgments xii
List of Contributors xiii
In Memoriam xiv
1 Introduction to E³ Models and Techniques in Aerospace Systems 1
Ira Kohlberg
1.1 Introduction and Topics of Interest 1
1.2 Autonomous Systems 8
1.3 Coupled Air and Space Survivable Systems 30
1.4 EMC Considerations of Chaos 41
1.5 EMC Effects on and Technology for Aerospace Systems 52
References 73
2 Deterministic and Statistical EMC Models for Field-to-Wire Coupling and Crosstalk in Wire Harness 79
Sergio Pignari
2.1 Introduction 79
2.2 DeterministicModeling 79
2.3 StatisticalModeling 99
References 115
3 HEMP Protection and Verification 121
William D. Prather
3.1 Introduction 121
3.2 High-Altitude Electromagnetic Pulse 122
3.3 HEMP Coupling to Aircraft 129
3.4 Shielding and Shielding Topology 133
3.5 EM Protection Technology 135
3.6 System-Level Specifications and Measurements 137
3.7 Hardening Component Specifications and Measurements 169
3.8 Hardness Maintenance/Hardness Surveillance 180
3.9 Conclusion 182
References 183
4 HIRF and Lightning Effects and Testing 187
Martin Gabrisak
4.1 Introduction 187
4.2 Coupling Analysis 190
4.3 HIRF Electromagnetic Environment and Its Effects 249
4.4 Electromagnetic Effects of Lightning 280
4.5 Precipitation Static (P-Static) 321
4.6 Lightning Effects and Protection in Aerospace 330
References 340
5 Techniques to Design Robust Lightning Protection Circuits for Avionics Equipment 347
Dr. ClayMcCreary
5.1 Introduction 347
5.2 Clean Sheet Design 347
5.3 Evaluating and Hardening Existing Protection 368
5.4 Design Examples 372
5.5 Conclusion 378
References 378
6 Pyrotechnic Systems in Aerospace Applications 381
Karen Burnham
6.1 Introduction 381
6.2 Component-Level Concerns 383
6.3 Vehicle-Level Concerns 390
6.4 Conclusion 404
References 404
7 Assembly-Level EMC Testing of Space Components/Subsystems 407
Leslie R.Warboys
7.1 Preliminary Steps 407
7.2 Basic Testing Concepts 408
7.3 Commonly Performed Tests 409
7.4 Test Plan 410
7.5 Testing Sequence 414
References 444
8 System-Level Testing of Spacecraft 445
JohannesWolf
8.1 Classification of System-Level Testing 445
8.2 System-Level Requirements Definition 452
8.3 Test Execution at the System Level 461
References 479
9 Subsystem EMC for Aircraft 483
Paul Kay
9.1 Introduction: The Aim of Subsystem-Level Testing 483
9.2 Motivations for Testing: Safety of Flight and Success of Mission 486
9.3 Emissions Tests 492
9.4 Immunity Tests 511
9.5 Test Plans for Avionics Subsystems 524
Further Reading 535
10 EMI Effects in Flight Control Systems and Their Mitigations 537
IrfanMajid
10.1 Introduction 538
10.2 Nature of EMI Experienced by Aerospace Vehicles 540
10.3 Reported Catastrophic EMI Occurrences in FCS 545
10.4 Anatomy of FBWFCS 548
10.5 Flight Management System 554
10.6 EMC Test Standards 556
10.7 EMC Test Methodologies of FCS 566
10.8 How EMI Couples to FCS 580
10.9 Modeling and Simulation 586
10.10 FCS of UAVs 590
10.11 Some Special Considerations f
Über den Autor / die Autorin
REINALDO J. PEREZ, PHD, MBA is a hardware and software engineer with 30 years of industrial experience in electronic engineering design and development, reliability engineering, electromagnetic compatibility, software engineering, and applied research. He has participated in the reliable design, development, manufacture and tests of avionics hardware for many aerospace applications at the board, assembly, subsystems, and system levels. He has been involved in IEEE for many years and has occupied many managerial and technical positions in IEEE. He has published extensively in peer reviewed journals and conferences in the fields of electrical, software, and aerospace engineering. He has taught as an adjunct several engineering disciplines at engineering colleges.
