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Flight control systems research. [optimization of f-8 aircraft control system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Whitaker, H. P. Baram, Y. Cheng, Y. |
| Copyright Year | 1973 |
| Description | Theoretical development is reported for the parameter optimization design technique needed for digital flight control system design. The results of an example case study applying the optimization technique for continuous systems to an F-8 aircraft feedback control system are presented. The concept of evolving the simplest system configuration that is capable of meeting a specified set of performance requirements is illustrated in this work. |
| File Size | 892162 |
| Page Count | 50 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740023314 |
| Archival Resource Key | ark:/13960/t1pg6fn27 |
| Language | English |
| Publisher Date | 1973-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Automatic Flight Control F-8 Aircraft Digital Systems Feedback Control Systems Engineering Optimal Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
