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Study of a control system to alleviate aircraft response to horizontal and vertical gusts. [for short takeoff aircraft with vane-controlled gust-alleviation system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Phillips, W. H. |
| Copyright Year | 1973 |
| Description | A study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-alleviation system. Effects of various combinations of design parameters on the responses to horizontal and vertical gusts and to elevator inputs are presented. Almost complete gust alleviation may be obtained with this system when the center of gravity of the STOL airplane is at rearward locations, but pitch stability augmentation is required for satisfactory control characteristics. |
| File Size | 931388 |
| Page Count | 40 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740003712 |
| Archival Resource Key | ark:/13960/t86h9b627 |
| Language | English |
| Publisher Date | 1973-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Aircraft Stability Aerodynamic Configurations Stabilization Gust Alleviators Aircraft Performance Short Takeoff Aircraft Feedback Control Flight Control Gust Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
