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Nonlinear control of aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Su, R. Hunt, L. R. Meyer, G. |
| Copyright Year | 1984 |
| Description | Transformations of nonlinear systems were used to design automatic flight controllers for vertical and short takeoff aircraft. Under the assumption that a nonlinear system can be mapped to a controllable linear system, a method using partial differential equations was constructed to approximate transformations in cases where exact ones cannot be found. An application of the design theory to a rotorcraft, the UH-1H helicopter, was presented. |
| File Size | 540194 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860019486 |
| Archival Resource Key | ark:/13960/t1gj4b85k |
| Language | English |
| Publisher Date | 1984-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Partial Differential Equations Automatic Flight Control Vectors Mathematics Mapping Helicopter Design Nonlinear Systems Matrices Mathematics Transformations Mathematics 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 |
