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Pilot-optimal multivariable control synthesis by output feedback
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schmidt, D. K. Innocenti, M. |
| Copyright Year | 1981 |
| Description | A control system design approach for optimal stability augmentation, systems, using limited state feedback theory with the specific inclusion of the human pilot in the loop is presented. The methodology is especially suitable for application to flight vehicles exhibiting nonconventional dynamic characteristics and for which quantitative handling qualities specifications are not available. The design is based on a correlation between pilot ratings and objective function of the optimal control model of the human pilot. Simultaneous optimization for augmentation and pilot gains are required. |
| File Size | 545067 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810019564 |
| Archival Resource Key | ark:/13960/t8qc4v28x |
| Language | English |
| Publisher Date | 1981-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Systems Management Pilot Performance Stability Optimal Control Light Modulation Aircraft Performance Control Theory Feedback Control Air Navigation 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 |
