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Digital adaptive flight controller development
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kotob, S. Kaufman, H. Alag, G. Berry, P. |
| Copyright Year | 1974 |
| Description | A design study of adaptive control logic suitable for implementation in modern airborne digital flight computers was conducted. Two designs are described for an example aircraft. Each of these designs uses a weighted least squares procedure to identify parameters defining the dynamics of the aircraft. The two designs differ in the way in which control law parameters are determined. One uses the solution of an optimal linear regulator problem to determine these parameters while the other uses a procedure called single stage optimization. Extensive simulation results and analysis leading to the designs are presented. |
| File Size | 3708572 |
| Page Count | 124 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750004895 |
| Archival Resource Key | ark:/13960/t1tf4k94h |
| Language | English |
| Publisher Date | 1974-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Digital Computers Fly By Wire Control Least Squares Method Probability Theory Feedback Control Parameterization Adaptive Control Aircraft Control 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 |
