#Worldshift system requirements install#
#Worldshift system requirements driver#
#Worldshift system requirements software#
#Worldshift system requirements download#

GNU* Bash is required for local installation and for setting up the environment to use the toolkit.įor CPU Host/Target Support Linux distrubtion for CPU Host/Target.

If you have Commercial Support, create a support ticket. If you have questions, access the Intel Community Forums when you need assistance. Note: These OS distributions are tested by Intel or known to work other distributions may or may not work and are not recommended.

#Worldshift system requirements install#

Please visit Installation Guide for Intel® oneAPI Toolkits ' Install Intel GPU Drivers' section for up to date information.

#Worldshift system requirements driver#

See the individual tool release notes for full details.įor developing applications for offloading to accelerators like GPU or FPGA, a specific version of GPU driver is required for the supported operating system. Individual tools may support additional operating systems and architecture configurations. The operating systems listed below are supported on Intel® 64 Architecture.

#Worldshift system requirements software#

For FPGA development, see Intel(R) DPC++ Compiler System Requirements.Ĭommon Software Requirements Operating System Requirements.

#Worldshift system requirements download#

NOTE: During the installation process, the installer may need up to 6 GB of additional temporary disk storage to manage the download and intermediate installation files.

Maximum of ~24 GB diskspace if installing all components.~3 GB of disk space (minimum) if only installing compiler and its libraries: Intel oneAPI DPC++/C++ Compiler, Intel® DPC++ Compatibility Tool, Intel® oneAPI DPC++ Library and Intel® Threading Building Block.FPGA Card: see Intel(R) DPC++ Compiler System Requirements.Integrated GEN9 or higher GPUs including latest Intel® Iris® Xe MAX graphics (DG1).Intel® Core™ processor family or higher.Systems based on Intel® 64 architectures below are supported both as host and target platforms. Common Hardware Requirements CPU Processor: For component level system requirements, please scroll down and click on each component link for details. This article contains the common system requirements for Intel® oneAPI Base Toolkit. From an airspace planning perspective, the experiment shows how strictly the trajectories over ground are maintained, despite some significant wind presence. The systems under investigation all met the required navigation performance and thus serve as a very nice example of how a performance-based requirement can be met by different techniques. The airframes involved very large (B747) and also rather small (Phenom 100) platforms and corresponding FMS manufacturers included a representative sample of the market. roll-rate, roll-acceleration), this is obviously influenced by the type of airframe and the capabilities of the respective flight control system. It is interesting to see, that not all manufacturers use the same commands (i.e. Bench test data was provided by the manufacturers, after they had been tasked with the same procedures. was able to compare several typical guidance system (FMS) and aircraft combinations with regard to their tracking performance during RF-legs. Some airworthiness authorities also require a flight technical error (FTE) analysis for consecutive reversing RF legs as well as for configuration changes during an RF leg.

The aircraft documentation shall contain limitations regarding the use of “direct-to” functionality in the context of RF legs (see below).

Īn electronic map displaying the selected procedure including RF legs shall be available to the flight crew. If this is not ensured, additional crew training to select NAV mode has to be specified. In case of go-around (TOGA application), the guidance mode should remain in NAV and not revert to HDG or TRK. The ability of the aircraft to maintain an RF leg after such a failure (e.g.: autopilot failure) shall be documented. Īny failure affecting the ability to execute RF legs shall be annunciated in the pilot’s primary field of view. The guidance/flight control system combination shall achieve the required accuracy using at least “roll-steering” capability. The guidance systems are required to be capable of commanding up to 30 degrees of bank above 400 ft agl for RNP procedures and also up to 8 degrees below 400 ft agl for RNP AR procedures. If this is not feasible, pilot training to identify and avoid RF legs is also accepted. The avionics shall not allow selection of a procedure that the aircraft is not capable of executing (e.g.: selection of a procedure containing RF legs, if the aircraft is not approved for such an operation).