PL441534A1 - Architektura zintegrowanego układu awioniki - Google Patents

Architektura zintegrowanego układu awioniki

Info

Publication number
PL441534A1
PL441534A1 PL441534A PL44153420A PL441534A1 PL 441534 A1 PL441534 A1 PL 441534A1 PL 441534 A PL441534 A PL 441534A PL 44153420 A PL44153420 A PL 44153420A PL 441534 A1 PL441534 A1 PL 441534A1
Authority
PL
Poland
Prior art keywords
processor
data
hardware
unit
units
Prior art date
Application number
PL441534A
Other languages
English (en)
Inventor
Mehmet Cemil KAZANBAS
Mehmet Fatih SAYARLAR
Sadik HOTMAN
Tolga SAYIN
Original Assignee
Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi filed Critical Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
Publication of PL441534A1 publication Critical patent/PL441534A1/pl

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/3003—Monitoring arrangements specially adapted to the computing system or computing system component being monitored
    • G06F11/3013—Monitoring arrangements specially adapted to the computing system or computing system component being monitored where the computing system is an embedded system, i.e. a combination of hardware and software dedicated to perform a certain function in mobile devices, printers, automotive or aircraft systems
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/0706—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment
    • G06F11/0736—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function
    • G06F11/0739—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation the processing taking place on a specific hardware platform or in a specific software environment in functional embedded systems, i.e. in a data processing system designed as a combination of hardware and software dedicated to performing a certain function in a data processing system embedded in automotive or aircraft systems
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/0703—Error or fault processing not based on redundancy, i.e. by taking additional measures to deal with the error or fault not making use of redundancy in operation, in hardware, or in data representation
    • G06F11/0751—Error or fault detection not based on redundancy
    • G06F11/0754—Error or fault detection not based on redundancy by exceeding limits
    • G06F11/076—Error or fault detection not based on redundancy by exceeding limits by exceeding a count or rate limit, e.g. word- or bit count limit
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
    • G06F11/3409—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment
    • G06F11/3433—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment for performance assessment for load management
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/30—Monitoring
    • G06F11/34—Recording or statistical evaluation of computer activity, e.g. of down time, of input/output operation ; Recording or statistical evaluation of user activity, e.g. usability assessment
    • G06F11/3466—Performance evaluation by tracing or monitoring
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F2201/00—Indexing scheme relating to error detection, to error correction, and to monitoring
    • G06F2201/81—Threshold

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Quality & Reliability (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Computing Systems (AREA)
  • Mathematical Physics (AREA)
  • Debugging And Monitoring (AREA)
  • Selective Calling Equipment (AREA)
  • Multi Processors (AREA)
  • Executing Machine-Instructions (AREA)
  • Small-Scale Networks (AREA)

Abstract

Zgłoszenie dotyczy wielu płyt elektronicznych (2), które przeprowadzają funkcje awioniki, które zapewniają zarządzanie i sterowanie lotem w pojazdach powietrznych i/lub kosmicznych, wielu jednostek (3) procesora na każdej płycie elektronicznej (2), które przetwarzają dane graficzne i arytmetyczne, uzyskane przez wejścia zapewniające dane ze środowiska fizycznego do płyty elektronicznej (2), co najmniej jednej sprzętowej jednostki (4) procesora na każdej płycie elektronicznej (2), która przetwarza dane ze środowiska fizycznego i zapewnia wyjście, przenosi przetworzone dane z jednostki (3) procesora do wyjścia, a następnie wysyła polecenia, które przeprowadzają funkcje awioniki, wielu jednostek (5) pamięci, które są umieszczone w połączeniu ze sprzętową jednostką (4) procesora, umożliwiając zapisywanie danych przetworzonych przez jednostki (3) procesora i danych nadawanych przez sprzętową jednostkę (4) procesora oraz umożliwiają zapisywanie danych przetworzonych przez sprzętową jednostkę (4) procesora, płyty nadzorującej (6), która jest umieszczona w połączeniu ze sprzętową jednostką (4) procesora i zapewnia konfigurację, za pomocą sprzętowych jednostek (4) procesora na płytach elektronicznych (2), dla których jest określany stan techniczny, jako wynik porównania danych wartości progowej określonej przez użytkownika dla poziomu obciążenia przetwarzania dla każdej płyty elektronicznej (2) z poziomami obciążenia przetwarzania.
PL441534A 2019-12-25 2020-12-23 Architektura zintegrowanego układu awioniki PL441534A1 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR2019/21508A TR201921508A2 (tr) 2019-12-25 2019-12-25 Bir birleştirilmiş aviyonik sistem mimarisi.
PCT/TR2020/051360 WO2021133346A1 (en) 2019-12-25 2020-12-23 An integrated avionic system architecture

Publications (1)

Publication Number Publication Date
PL441534A1 true PL441534A1 (pl) 2022-12-05

Family

ID=76574954

Family Applications (1)

Application Number Title Priority Date Filing Date
PL441534A PL441534A1 (pl) 2019-12-25 2020-12-23 Architektura zintegrowanego układu awioniki

Country Status (6)

Country Link
KR (1) KR20220115972A (pl)
AU (1) AU2020414291A1 (pl)
BR (1) BR112022012675A2 (pl)
PL (1) PL441534A1 (pl)
TR (1) TR201921508A2 (pl)
WO (1) WO2021133346A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102665431B1 (ko) * 2023-11-21 2024-05-10 국방과학연구소 멀티코어 프로세서 기반 항공전자컴퓨터 장치에 구비된 응용 소프트웨어의 실행에 대한 정보를 재설정하는 장치 및 방법

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2946769B1 (fr) * 2009-06-16 2011-07-01 Airbus France Procede et dispositif de reconfiguration d'avionique.
WO2012158081A1 (en) * 2011-05-17 2012-11-22 Saab Ab Distributed avionics system and method for backup handling in an avionics system
US20130181809A1 (en) * 2011-07-27 2013-07-18 Michael R. Lin SpaceCube MINI

Also Published As

Publication number Publication date
KR20220115972A (ko) 2022-08-19
AU2020414291A1 (en) 2022-08-11
TR201921508A2 (tr) 2021-07-26
BR112022012675A2 (pt) 2022-09-06
WO2021133346A1 (en) 2021-07-01

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