PL441534A1 - Architektura zintegrowanego układu awioniki - Google Patents
Architektura zintegrowanego układu awionikiInfo
- 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
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR 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; CALCULATING OR 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; CALCULATING OR 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; CALCULATING OR 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; CALCULATING OR 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; CALCULATING OR 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)
- Small-Scale Networks (AREA)
- Multi Processors (AREA)
- Executing Machine-Instructions (AREA)
- Selective Calling Equipment (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.
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)
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)
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. |
US20140157041A1 (en) * | 2011-05-17 | 2014-06-05 | 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 |
-
2019
- 2019-12-25 TR TR2019/21508A patent/TR201921508A2/tr unknown
-
2020
- 2020-12-23 PL PL441534A patent/PL441534A1/pl unknown
- 2020-12-23 KR KR1020227022272A patent/KR20220115972A/ko unknown
- 2020-12-23 WO PCT/TR2020/051360 patent/WO2021133346A1/en active Application Filing
- 2020-12-23 AU AU2020414291A patent/AU2020414291A1/en active Pending
- 2020-12-23 BR BR112022012675A patent/BR112022012675A2/pt unknown
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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