Validation of an Integrated Airframe and Turbofan Engine Simulation for Evaluation of Propulsion Control Modes
Validation of an Integrated Airframe and Turbofan Engine Simulation for Evaluation of Propulsion Control Modes
- New search for: Litt, Jonathan
- New search for: Sowers, T Shane
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- New search for: Guo, Ten-Huei
- New search for: Litt, Jonathan
- New search for: Sowers, T Shane
- New search for: Liu, Yuan
- New search for: Owen, A. Karl
- New search for: Guo, Ten-Huei
The National Aeronautics and Space Administration (NASA) has developed independent airframe and engine models that have been integrated into a single real-time aircraft simulation for piloted evaluation of propulsion control algorithms. In order to have confidence in the results of these evaluations, the integrated simulation must be validated to demonstrate that its behavior is realistic and that it meets the appropriate Federal Aviation Administration (FAA) certification requirements for aircraft. The paper describes the test procedures and results, demonstrating that the integrated simulation generally meets the FAA requirements and is thus a valid testbed for evaluation of propulsion control modes.
Document information
Validation of an Integrated Airframe and Turbofan Engine Simulation for Evaluation of Propulsion Control Modes
SciTech 2015 ; 2015 ; Kissimmee, FL, United States
2015-01-05
Conference paper
No indication
English
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