Analysis of Spacecraft System-Level Electromagnetic Compatibility

In the previous sections, the design requirements and analysis methods of bonding, grounding, shielding, and cable layout in the electromagnetic environmental effects (EME) of spacecraft systems were described. Starting from the aspects of EMI margin, intra-system electromagnetic compatibility (EMC), the hazards of electromagnetic radiation to personnel and electric explosive devices (EED), etc., and electromagnetic spectrum compatibility, this chapter mainly addresses the basic methods and processes of analysis.