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Altitude response of several airplanes during landing approach. [including space shuttle
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Phillips, W. H. |
| Copyright Year | 1979 |
| Description | The response in altitude and pitching velocity of the shuttle and of four other airplanes during the landing approach is compared. The effects of airplane type, pitch damping, center-of-gravity location, lift coefficient, and cockpit position are presented. The reasons for the differences observed and the effects of these differences on control characteristics are discussed. |
| File Size | 1209779 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800005882 |
| Archival Resource Key | ark:/13960/t1gj4997k |
| Language | English |
| Publisher Date | 1979-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Aircraft Landing Transfer Functions Delta Wings Center of Gravity Approach Altitude Control Aerodynamic Coefficients Laplace Transformation Space Shuttle Orbiters Aircraft Configurations Stability Derivatives Lift 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 |
