NASA Technical Reports Server (NTRS) 19980232012: The Effects Of Longitudinal Control-System Dynamics On Pilot Opinion And Response Characteristics As Determined From Flight Tests And From Ground Simulator Studies - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19980232012: The Effects Of Longitudinal Control-System Dynamics On Pilot Opinion And Response Characteristics As Determined From Flight Tests And From Ground Simulator Studies" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19980232012: The Effects Of Longitudinal Control-System Dynamics On Pilot Opinion And Response Characteristics As Determined From Flight Tests And From Ground Simulator Studies” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19980232012: The Effects Of Longitudinal Control-System Dynamics On Pilot Opinion And Response Characteristics As Determined From Flight Tests And From Ground Simulator Studies
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19980232012
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"NASA Technical Reports Server (NTRS) 19980232012: The Effects Of Longitudinal Control-System Dynamics On Pilot Opinion And Response Characteristics As Determined From Flight Tests And From Ground Simulator Studies" Description:
The Internet Archive:
The results of a fixed-base simulator study of the effects of variable longitudinal control-system dynamics on pilot opinion are presented and compared with flight-test data. The control-system variables considered in this investigation included stick force per g, time constant, and dead-band, or stabilizer breakout force. In general, the fairly good correlation between flight and simulator results for two pilots demonstrates the validity of fixed-base simulator studies which are designed to complement and supplement flight studies and serve as a guide in control-system preliminary design. However, in the investigation of certain problem areas (e.g., sensitive control-system configurations associated with pilot- induced oscillations in flight), fixed-base simulator results did not predict the occurrence of an instability, although the pilots noted the system was extremely sensitive and unsatisfactory. If it is desired to predict pilot-induced-oscillation tendencies, tests in moving-base simulators may be required. It was found possible to represent the human pilot by a linear pilot analog for the tracking task assumed in the present study. The criterion used to adjust the pilot analog was the root-mean-square tracking error of one of the human pilots on the fixed-base simulator. Matching the tracking error of the pilot analog to that of the human pilot gave an approximation to the variation of human-pilot behavior over a range of control-system dynamics. Results of the pilot-analog study indicated that both for optimized control-system dynamics (for poor airplane dynamics) and for a region of good airplane dynamics, the pilot response characteristics are approximately the same.
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