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  • 1
    Electronic Resource
    Electronic Resource
    Directions in the Anthropology of Contemporary Japan (1991)
    Palo Alto, Calif. : Annual Reviews
    Annual Review of Anthropology 20 (1991), S. 395-431 
    Details
    ISSN: 0084-6570
    Source: Annual Reviews Electronic Back Volume Collection 1932-2001ff
    Topics: Ethnic Sciences , Biology
    Type of Medium: Electronic Resource
    URL: http://dx.doi.org/10.1146/annurev.an.20.100191.002143
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    Paper (German National Licenses)
    Fulltext
  • 2
    facet.materialart.
    Unknown
    Velocity vector control system augmented with direct lift control (1981)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A pilot-controlled stability control system that employs direct lift control (spoiler control) with elevator control to control the flight path angle of an aircraft is described. A computer on the aircraft generates an elevator control signal and a spoiler control signal, using a pilot-controlled pitch control signal and pitch rate, vertical velocity, roll angle, groundspeed, engine pressure ratio and vertical acceleration signals which are generated on the aircraft. The direct lift control by the aircraft spoilers improves the response of the aircraft flight path angle and provides short term flight path stabilization against environmental disturbances.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Unknown
    Simulator results of an F-14A airplane utilizing an aileron-rudder interconnect during carrier approaches and landings (1980)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: A piloted simulator study was conducted to evaluate an aileron rudder interconnect (ARI) control system for the F-14A airplane in the landing configuration. Effects on pilot performance and handling characteristics were investigated. Two ARI configurations were tested and compared to the standard F-14 fleet control system. A nonlinear aerodynamic model of the F-14 was used in conjunction with a six degree of freedom motion base simulator. The evaluation task, which utilized three subject pilots, consistent of a night carrier approach and landing. Both ARI configurations produced improved pilot performance and pilot ratings when compared to the standard control system. Sideslip due to adverse yaw as considerably reduced by the ARI systems and heading control was more stable and precise. Lateral deviation from centerline was reduced during the approach and lateral touchdown dispersion on the carrier deck was reduced with the ARI control systems.
    Keywords: AIRCRAFT STABILITY AND CONTROL
    Type: NASA-TM-81833
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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