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Dynamics and identification of flexible aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wells, W. R. |
| Copyright Year | 1976 |
| Description | The equations of motion and a maximum likelihood parameter identification formulation are developed for a flexible aircraft. The various levels of approximation associated with the modal substitution representation of the elastic displacement field are discussed and illustrated when appropriate. The necessary extension of the parameter set of stability and control derivatives due to the aeroelastic effects is obtained. |
| File Size | 1225977 |
| Page Count | 69 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760014070 |
| Archival Resource Key | ark:/13960/t6450g30j |
| Language | English |
| Publisher Date | 1976-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Flexible Bodies Control Stability Modulus of Elasticity Identifying Equations of Motion Aircraft Structures Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |