WO2016102055A3 - Method for operating a control component for an aircraft and control component - Google Patents
Method for operating a control component for an aircraft and control component Download PDFInfo
- Publication number
- WO2016102055A3 WO2016102055A3 PCT/EP2015/002542 EP2015002542W WO2016102055A3 WO 2016102055 A3 WO2016102055 A3 WO 2016102055A3 EP 2015002542 W EP2015002542 W EP 2015002542W WO 2016102055 A3 WO2016102055 A3 WO 2016102055A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- control component
- aircraft
- operating
- processor
- applications
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/46—Multiprogramming arrangements
- G06F9/48—Program initiating; Program switching, e.g. by interrupt
- G06F9/4806—Task transfer initiation or dispatching
- G06F9/4843—Task transfer initiation or dispatching by program, e.g. task dispatcher, supervisor, operating system
- G06F9/4881—Scheduling strategies for dispatcher, e.g. round robin, multi-level priority queues
- G06F9/4887—Scheduling strategies for dispatcher, e.g. round robin, multi-level priority queues involving deadlines, e.g. rate based, periodic
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/46—Multiprogramming arrangements
- G06F9/50—Allocation of resources, e.g. of the central processing unit [CPU]
- G06F9/5061—Partitioning or combining of resources
- G06F9/5066—Algorithms for mapping a plurality of inter-dependent sub-tasks onto a plurality of physical CPUs
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/64—Hybrid switching systems
- H04L12/6418—Hybrid transport
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L12/00—Data switching networks
- H04L12/28—Data switching networks characterised by path configuration, e.g. LAN [Local Area Networks] or WAN [Wide Area Networks]
- H04L12/40—Bus networks
- H04L2012/40267—Bus for use in transportation systems
- H04L2012/4028—Bus for use in transportation systems the transportation system being an aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Software Systems (AREA)
- Theoretical Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Hardware Redundancy (AREA)
- Multi Processors (AREA)
- Safety Devices In Control Systems (AREA)
- Control By Computers (AREA)
Abstract
The invention relates to a method for operating a control component for an aircraft on the basis of a software framework comprising at least one multicore processor for parallel execution of safety-critical avionics applications, the processor architecture comprising at least one system bus and at least one separate peripheral bus, and applications being executed in parallel on two or more application processor cores and access to the peripheral bus being managed by a dedicated I/O processor core.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102014019531.7A DE102014019531A1 (en) | 2014-12-23 | 2014-12-23 | Method for operating an aircraft control component and control component |
DE102014019531.7 | 2014-12-23 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2016102055A2 WO2016102055A2 (en) | 2016-06-30 |
WO2016102055A3 true WO2016102055A3 (en) | 2016-09-22 |
Family
ID=55173816
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2015/002542 WO2016102055A2 (en) | 2014-12-23 | 2015-12-16 | Method for operating a control component for an aircraft and control component |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE102014019531A1 (en) |
WO (1) | WO2016102055A2 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3071334B1 (en) * | 2017-09-19 | 2019-08-30 | Psa Automobiles Sa | METHOD FOR ENSURING DATA STABILITY OF A MULTICOAL PROCESSOR OF A MOTOR VEHICLE |
US11254441B2 (en) * | 2018-11-29 | 2022-02-22 | Hamilton Sundstrand Corporation | Aircraft controller including multiple core processor with wireless transmission prognostic/diagnostic data capability |
US11097857B2 (en) * | 2018-11-30 | 2021-08-24 | Hamilton Sundstrand Corporation | Multiple core motor controller processor with embedded prognostic/diagnostic capabilities |
CN110597754B (en) * | 2019-08-02 | 2023-02-21 | 北京多思安全芯片科技有限公司 | Master-slave type safety processor |
CN110781055B (en) * | 2019-10-15 | 2023-03-10 | 中国航空无线电电子研究所 | Service component running state monitoring method of embedded partition real-time operating system |
DE102020213371A1 (en) | 2020-10-22 | 2022-04-28 | Robert Bosch Gesellschaft mit beschränkter Haftung | Device and method for controlling a technical system |
CN112241352B (en) * | 2020-11-03 | 2023-10-20 | 中国航空工业集团公司西安航空计算技术研究所 | Monitoring system of gridding fault-tolerant computer platform |
DE102021209627A1 (en) | 2021-09-01 | 2023-03-02 | Robert Bosch Gesellschaft mit beschränkter Haftung | System and method for running functionally identical applications |
CN115509986B (en) * | 2022-09-28 | 2024-05-07 | 美的集团(上海)有限公司 | Inter-core communication method, electronic device, and storage medium |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011159209A1 (en) * | 2010-06-17 | 2011-12-22 | Saab Ab | Distributed avionics |
-
2014
- 2014-12-23 DE DE102014019531.7A patent/DE102014019531A1/en active Pending
-
2015
- 2015-12-16 WO PCT/EP2015/002542 patent/WO2016102055A2/en active Application Filing
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011159209A1 (en) * | 2010-06-17 | 2011-12-22 | Saab Ab | Distributed avionics |
Also Published As
Publication number | Publication date |
---|---|
DE102014019531A1 (en) | 2016-06-23 |
WO2016102055A2 (en) | 2016-06-30 |
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