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Failure detection and identification for a reconfigurable flight control system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Dallery Sr., Francois |
| Copyright Year | 1987 |
| Description | Failure detection and identification logic for a fault-tolerant longitudinal control system were investigated. Aircraft dynamics were based upon the cruise condition for a hypothetical transonic business jet transport configuration. The fault-tolerant control system consists of conventional control and estimation plus a new outer loop containing failure detection, identification, and reconfiguration (FDIR) logic. It is assumed that the additional logic has access to all measurements, as well as to the outputs of the control and estimation logic. The pilot may also command the FDIR logic to perform special tests. |
| File Size | 149968 |
| Page Count | 5 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870009096 |
| Archival Resource Key | ark:/13960/t8hf2qq7c |
| Language | English |
| Publisher Date | 1987-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Fault Tolerance Transport Aircraft Failure Analysis Jet Aircraft Mathematical Logic Applications Programs Computers Flight Control Kalman Filters Fortran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
