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Moving base simulation evaluation of translational rate command systems for stovl aircraft in hover
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Franklin, James A. Stortz, Michael W. |
| Copyright Year | 1996 |
| Description | Using a generalized simulation model, a moving-base simulation of a lift-fan short takeoff/vertical landing fighter aircraft has been conducted on the Vertical Motion Simulator at Ames Research Center. Objectives of the experiment were to determine the influence of system bandwidth and phase delay on flying qualities for translational rate command and vertical velocity command systems. Assessments were made for precision hover control and for landings aboard an LPH type amphibious assault ship in the presence of winds and rough seas. Results obtained define the boundaries between satisfactory and adequate flying qualities for these design features for longitudinal and lateral translational rate command and for vertical velocity command. |
| File Size | 1301321 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19960042888 |
| Archival Resource Key | ark:/13960/t48q0z75r |
| Language | English |
| Publisher Date | 1996-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Vertical Motion Simulators Flight Characteristics Stovl Aircraft Vertical Landing V/stol Aircraft Command Guidance Flight Control Hovering Flight Simulation 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 |
