Piloted simulation evaluation of pitch control designs for highly augmented STOVL aircraftAnalyses of design variations on a pitch axis stabilization and command augmentation system (SCAS) for a STOVL fighter aircraft are performed in a moving base simulation experiment. The primary goal of this study is to determine if turbulence-induced control activity could be reduced by modifying SCAS parameters while keeping the response-to-command characteristics of the baseline system that provide Level 1 flying qualities. Pilot ratings and control utilization statistics for the baseline system are in agreement with similar data gathered in a prior simulation test involving the same aircraft and control system.
Document ID
19930029331
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Engelland, S. A. (NASA Ames Research Center Moffett Field, CA, United States)
Franklin, J. A. (NASA Ames Research Center Moffett Field, CA, United States)
Stortz, M. W. (NASA Ames Research Center Moffett Field, CA, United States)
Hardy, G. H. (NASA Ames Research Center Moffett Field, CA, United States)