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Interactive aircraft flight control and aeroelastic stabilization
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schmidt, D. K. Weisshaar, T. A. |
| Copyright Year | 1984 |
| Description | The potential benefits and costs of optimizing both the structural stiffness and the active control of aircraft in a rational manner are investigated. The ultimate goal is to arrive at a unified treatment of structural and active control design for the stability augmentation of flexible aircraft. An exhaustive literature evaluation in the area of passive tailoring for aircraft performance is undertaken. A mathematical technique to be used for aeroservoelastic tailoring studies is described. Two analytical models, one elementary, the other sophisticated, are developed to illustrate the potential for aeroservoelastic tailoring. Both models have essential features of real world hardware, yet the physical understanding is not buried in a myriad of detail. These models are also described. |
| File Size | 4173065 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840023144 |
| Archival Resource Key | ark:/13960/t9v16w285 |
| Language | English |
| Publisher Date | 1984-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Flexible Bodies Structural Stability Servocontrol Aircraft Design Feedback Control Perturbation Equations of Motion Optimization Flight Characteristics Mathematical Models Stiffness Active Control Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |