Ways to achieve helicopter digital flight control system reliability and survivability are shown. Microcomputer system failures caused by electromagnetic interference (EMI) and their impact on flight control are considered. Ways to ensure self recovery after EMI induced faults are outlined. A digital flight control system designed with respect to EMI problems and flight tested on a BK-117 is presented.
Electromagnetic Interference (EMI) Fault Prevention and Self Recovery of Digital Flight Control Systems
1986
20 pages
Report
Keine Angabe
Englisch
On Upsets of Analog Portions of Digital Flight Control Systems Due to Electromagnetic Interference
SAE Technical Papers | 1991
|British Library Conference Proceedings | 2000
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