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Flight evaluation of an integrated control and display system for high-precision manual landing flare of powered-lift STOL aircraftAn account is given of the features and performance of a manual landing flare and touchdown system capable of great precision, as demonstrated by its installation in the NASA Quiet Short-haul Research Aircraft (QSRA). The integrated cockpit display and closed-loop control employed constitutes a trajectory-augmentation system that extends QSRA flight control from augmentation of altitude, flight path angle, and airspeed, to the augmentation of the trajectory itself. The + or - 18 ft touchdown dispersion achieved is approximately equal to that obtained during aircraft carrier trials of the same aircraft.
Document ID
19880049960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hynes, Charles S.
(NASA Ames Research Center Moffett Field, CA, United States)
Hardy, Gordon H.
(NASA Ames Research Center Moffett Field, CA, United States)
Kaisersatt, Thomas J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
SAE PAPER 872316
Meeting Information
Meeting: International Powered Lift Conference and Exposition
Location: Santa Clara, CA
Country: United States
Start Date: December 7, 1987
End Date: December 10, 1987
Sponsors: SAE, DOT, DOD, and NASA.
Accession Number
88A37187
Distribution Limits
Public
Copyright
Other

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