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Fail-operational fault tolerant flight critical computer architecture and monitoring method

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G06F-011/16
출원번호 US-0054777 (1993-04-27)
발명자 / 주소
  • Hay Rick H. (Cave Creek AZ) Smith Clarence S. (Glendale AZ) Girts Robert D. (Mesa AZ) Yount Larry J. (Scottsdale AZ)
출원인 / 주소
  • Honeywell Inc. (Minneapolis MN 02)
인용정보 피인용 횟수 : 65  인용 특허 : 0

초록

A flight critical computer system for an aircraft includes dual independent lanes having two processors in each lane. The first lane has a primary processor and a redundant processor and provides a first command signal. The second lane includes a primary processor and a redundant processor and provi

대표청구항

A flight critical computer system for an aircraft, the aircraft having sensor means for providing sensor signals representative of characteristics concerning the aircraft, said system comprising: a first lane having a first primary processor and a first redundant processor and for providing a first

이 특허를 인용한 특허 (65)

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  4. Larry J. Yount, Critical control adaption of integrated modular architecture.
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