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Performance analysis of flexible aircraft with active control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Noll, R. B. Morino, L. |
| Copyright Year | 1976 |
| Description | Small perturbation equations of motion of a flexible aircraft with an active control technology (ACT) system were developed to evaluate the stability and performance of the controlled aircraft. The total aircraft system was formulated in state vector format and the system of equations was completed with fully unsteady and low frequency aerodynamics for arbitrary, complex configurations based on a potential aerodynamic method. The ACT system equations were incorporated in the digital computer program FCAP (Flight Control Analysis Program) which can be used for the analysis of complete aircraft configurations, including control system, with either low frequency or fully unsteady aerodynamics. The application of classical performance analyses including frequency response, poles and zeros, mean square response, and time response in FCAP in state vector format was discussed. |
| File Size | 371340 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770003436 |
| Archival Resource Key | ark:/13960/t6xw96k66 |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Perturbation Theory Digital Computers Flexible Bodies Performance Tests Unsteady Aerodynamics Mathematical Models Equations of Motion Low Frequencies Air Navigation 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 | Article |
