The purpose of this contract was to develop a computerized method for analyzing electromagnetic compatibility on aerospace vehicles. The analysis has four sections resulting in four computer programs which can be run together or independently. Each program analyzes a different coupling path between avionics subsystems on the air vehicle. The paths are antenna-to-antenna, wire-to-wire, electromagnetic field-to-wire, and box-to-box coupling. This is Part II of a three part report. This part describes tests to validate each analysis. Test objectives, setups, and procedures are given as well as test results. These results are compared to the corresponding calculated predictions from the programs. For each program, conclusions, applications, limitations, and recommendations are also provided. (Author)
Intra-Vehicle Electromagnetic Compatibility Analysis. Part II. Computer Program Validation Tests
1971
70 pages
Report
Keine Angabe
Englisch
Radiofrequency Waves , Aircraft , Computer Hardware , Electromagnetic compatibility , Computer programming , Aircraft equipment , Aircraft antennas , Circuits , Electromagnetic fields , Electromagnetic shielding , Test methods , Reliability(Electronics) , Jet fighters , Jet transport planes , Avionics , C-135 aircraft , F-4 aircraft , F-4e aircraft , Kc-135 aircraft
Computer modelling for vehicle electromagnetic compatibility
Tema Archiv | 1988
|Electromagnetic compatibility tests for multirotor UAS
IEEE | 2015
|Electromagnetic Compatibility in the Off-Highway Vehicle Part II: Electromagnetic Immunity (EMI)
SAE Technical Papers | 1992
|Electromagnetic Compatibility in the Off-Highway Vehicle Part III: Electromagnetic Emissions (EME)
SAE Technical Papers | 1992
|