Difference between revisions of "Airbus HIL Test Stands"
(Created page with "*Airbus A440M, A320, A340 and A350 HLSS HIL simulation. *Testing, verification and validation of the Airbus High Lift System used to control of wing flaps that generate high lif...") |
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*Testing, verification and validation of the Airbus High Lift System used to control of wing flaps that generate high lift during takeoff and landing. | *Testing, verification and validation of the Airbus High Lift System used to control of wing flaps that generate high lift during takeoff and landing. | ||
*Seamless integration with MathWorks Simulink for rapid model-based simulation. | *Seamless integration with MathWorks Simulink for rapid model-based simulation. | ||
− | + | *Thousands of I/O points and Simulink variables accessible via the SIMWB Real-time Data Base. | |
*All operations occur in real-time within a 500 microsecond frame time. | *All operations occur in real-time within a 500 microsecond frame time. |
Latest revision as of 17:44, 18 November 2011
- Airbus A440M, A320, A340 and A350 HLSS HIL simulation.
- Testing, verification and validation of the Airbus High Lift System used to control of wing flaps that generate high lift during takeoff and landing.
- Seamless integration with MathWorks Simulink for rapid model-based simulation.
- Thousands of I/O points and Simulink variables accessible via the SIMWB Real-time Data Base.
- All operations occur in real-time within a 500 microsecond frame time.