Application migration from linux prototype to deployable ima platform using arinc 653 and open gl

Kinnan, L.

doi:10.1109/dasc.2007.4391958

Cited by 7 publications

(5 citation statements)

References 1 publication

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“…Compared with the conventional Labview [7] and Open GL [8] methods, the virtual instrument developed by means of GL Studio [9] is more accurate, flexible and transplantable [10] [11]. With GL Studio, the development of simulation system will also be much easier and quicker [12].…”

Section: A Gl Studiomentioning

confidence: 99%

Simulation System for Airborne Weather Radar Control and Display Based on Virtual Instrument

Ruan¹,

Li²,

Yu³

2014

JSW

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A simulation system consisting of display module, control module and process module for the control and display unit(CDU) of airborne weather radar is designed and tested in this paper. Taking advantage of virtual instrument technology as well as practical aeronautical characteristics, the designed system can receive, process and intuitively reflect the meteorological information to fight crews. Adopting the function and algorithm multiplexing, the comprehensive and integrated system is successfully realized with efficiency and fidelity, in which major workings modes of practical weather radar including weather mode, windshear mode, turbulence mode and map mode are provided. The testing results indicate the system performs favorable interactivity, stability and real-time property which meet the requirements of simulation. The system can be widely used for training and teaching and is transplantable to similar simulation systems.

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Section: A Gl Studiomentioning

confidence: 99%

Simulation System for Airborne Weather Radar Control and Display Based on Virtual Instrument

Ruan¹,

Li²,

Yu³

2014

JSW

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“…Porting applications to one of the RTOS one might be using (RTEMS [2], eCos [3], VxWorks [4], etc.) can be a complicated task, and definitely not an error-free one [9], [10]. Furthermore, certain hardware interfaces may be necessary that are not supported by the given RTOS.…”

Section: Integration Of Generic Operating Systemsmentioning

confidence: 99%

Embedded Linux in a partitioned architecture for aerospace applications

Craveiro

Rufino

Almeida

et al. 2009

2009 IEEE/ACS International Conference on Computer Systems and Applications

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The ARINC 653 specification, defined for aeronautical applications, has the goal of providing a standard interface between a given real-time operating system (RTOS) and the corresponding applications. It also provides robust partitioning, with the final goal of guaranteeing safety and timeliness in mission-critical systems. The interest in ARINC 653 has extended to the aerospace industry, which resulted in the definition of an architecture, compliant with the specification, allowing for operating system heterogeneity. In this paper, we introduce the problem of integrating generic operating systems onto this architecture, and explore the case of GNU/Linux. Adding GNU/Linux allows running existing applications or interpreted scripts without needing to port the application or interpreter to an RTOS. In embedded systems, we have to cope with scarce resources and diverse existent hardware, and a balance between both issues must be reached. For such, we show the genesis of such a solution.

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Section: Introductionmentioning

confidence: 99%

“…Virtual integration involves integration between software components, and instances. To support this different software architecture, software platforms (RTOS) are used to provide partition mechanism, hardware resource management like CPU, Memory, input-output, interface between functionalities, communication mechanism, protocols between software components, networking methods using network stacks and concepts like TCP/IP protocol (Kinnan, Larry M. 2007). The virtual integration comes under the Product Systems Engineering (PSE), which focusses on the design, development and enhancement using RTOS, which plays a very important role in implementing system engineering principles like considering budget and schedule constraints, phase by phase development, model based development, easy to test, easy to integrate, easy to add new features, easy to modify architecture etc.…”

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confidence: 99%

Virtual Integration in Avionics Systems‐RTOS

Kouty¹,

Mishra²

2019

INCOSE International Symp

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This paper discuss about the challenges and thoughts in Virtual integration using Real Time Operating Systems for avionics system integration with respect to different architectures like Open System Architecture and Integrated Modular Avionics. This paper mainly discusses about role of RTOS like ARINC653 in solving the problems in Avionics System Engineering, in which software‐software integration and hardware‐software integration is achieved using features of RTOS and this approach is called Virtual Integration. I have proposed customization of existing RTOS using new concepts which enhances the capability of performance and extendibility in integration keeping core System Engineering Principles in mind. This paper discusses about the system integration challenges identified in use of existing RTOS which includes: 1. Cross Platform Development, 2. Selection of communication mechanisms and scheduling for mixed operating system environment, 3. Current RTOS are mainly Monolithic and Micro Kernel based to compete in speed of execution and process management. 4. Current RTOS are limited to target platforms like Power PC, Intel x86 etc. and not supporting soft processors like micro‐blaze, FPGA platforms etc. Proposal for future enhancements to include use of Kernel level scheduling algorithms and Nano Kernels in RTOS to host more Platform OS to have more number of independent process running with more accurate time scheduling with less switch overheads, support for cross platform development with different host development technologies, support for SOC, POC other than conventional processors like x86, Power PC, ARM and MIPS etc. This paper discusses about the Network Virtualization and its application in avionics integration to overcome the capability of hardware networking devices using RTOS. Applying Trusted Execution Technology (TXT) approach in Integrated Modular Avionics (IMA) to ensure that the launching components at BIOS, OS Loader and Hypervisor are safe and trusted to avoid failure and malfunctions during run‐time.

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Application migration from linux prototype to deployable ima platform using arinc 653 and open gl

Cited by 7 publications

References 1 publication

Simulation System for Airborne Weather Radar Control and Display Based on Virtual Instrument

Simulation System for Airborne Weather Radar Control and Display Based on Virtual Instrument

Embedded Linux in a partitioned architecture for aerospace applications

Virtual Integration in Avionics Systems‐RTOS

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