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High stability engine control (histec) flight test results
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gallops, George W. Orme, John S. Welsh, Mark G. Southwick, Robert D. DeLaat, John C. Kielb, Robert P. Kerr, Laura J. |
| Copyright Year | 1998 |
| Description | The High Stability Engine Control (HISTEC) Program, managed and funded by the NASA Lewis Research Center, is a cooperative effort between NASA and Pratt & Whitney (P&W). The program objective is to develop and flight demonstrate an advanced high stability integrated engine control system that uses real-time, measurement-based estimation of inlet pressure distortion to enhance engine stability. Flight testing was performed using the NASA Advanced Controls Technologies for Integrated Vehicles (ACTIVE) F-15 aircraft at the NASA Dryden Flight Research Center. The flight test configuration, details of the research objectives, and the flight test matrix to achieve those objectives are presented. Flight test results are discussed that show the design approach can accurately estimate distortion and perform real-time control actions for engine accommodation. |
| File Size | 878689 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19980211493 |
| Archival Resource Key | ark:/13960/t4hn05m45 |
| Language | English |
| Publisher Date | 1998-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Oscillating Flow Flight Tests Flow Distortion Inlet Pressure Fluid Flow Pressure Distribution Engine Control Aerodynamic Coefficients Thrust Control Aircraft Engines F-15 Aircraft Real Time Operation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
