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Development of an advanced pitch active control system for a wide body jet aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, Walt J. Guinn, Wiley A. Rising, Jerry J. |
| Copyright Year | 1984 |
| Description | An advanced PACS control law was developed for a commercial wide-body transport (Lockheed L-1011) by using modern control theory. Validity of the control law was demonstrated by piloted flight simulation tests on the NASA Langley visual motion simulator. The PACS design objective was to develop a PACS that would provide good flying qualities to negative 10 percent static stability margins that were equivalent to those of the baseline aircraft at a 15 percent static stability margin which is normal for the L-1011. Also, the PACS was to compensate for high-Mach/high-g instabilities that degrade flying qualities during upset recoveries and maneuvers. The piloted flight simulation tests showed that the PACS met the design objectives. The simulation demonstrated good flying qualities to negative 20 percent static stability margins for hold, cruise and high-speed flight conditions. Analysis and wind tunnel tests performed on other Lockheed programs indicate that the PACS could be used on an advanced transport configuration to provide a 4 percent fuel savings which results from reduced trim drag by flying at negative static stability margins. |
| File Size | 10546716 |
| Page Count | 163 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870008280 |
| Archival Resource Key | ark:/13960/t7zm0608z |
| Language | English |
| Publisher Date | 1984-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Static Stability Aircraft Fuels Control Systems Design Jet Aircraft Cost Reduction Pitch Inclination Flight Characteristics Longitudinal Control Wind Tunnel Tests Lockheed Aircraft Active Control Flight Simulation Mach Number 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 |
