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Moving base simulation of an integrated flight and propulsion control system for an ejector-augmentor stovl aircraft in hover
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | McNeill, Walter, E. Stortz, Michael W. Chung, William W. |
| Copyright Year | 1995 |
| Description | A piloted motion simulator evaluation, using the NASA Ames Vertical Motion Simulator, was conducted in support of a NASA Lewis Contractual study of the integration of flight and propulsion systems of a STOVL aircraft. Objectives of the study were to validate the Design Methods for Integrated Control Systems (DMICS) concept, to evaluate the handling qualities, and to assess control power usage. The E-7D ejector-augmentor STOVL fighter design served as the basis for the simulation. Handling-qualities ratings were obtained during precision hover and shipboard landing tasks. Handling-qualities ratings for these tasks ranged from satisfactory to adequate. Further improvement of the design process to fully validate the DMICS concept appears to be warranted. |
| File Size | 1554006 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950024225 |
| Archival Resource Key | ark:/13960/t5fc00h6m |
| Language | English |
| Publisher Date | 1995-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Stovl Aircraft Aircraft Landing Flight Control Powered Lift Aircraft Hovering Aircraft Control Vertical Motion Simulators Flight Simulators Aircraft Carriers Propulsion Controllability Lateral Control Fighter Aircraft Flight Simulation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
