Author: Malcolm L. RitchiePublisher:
ISBN:
Category : Aeronautical instruments
Languages : en
Pages : 34
Book Description
"Mounting the gyroscopic turn indicator on the sloping panel of an all-weather interceptor resulted in negative quickening of the display indication. Experiments in an electronic flight simulator demonstrated the adverse effect of negative quickening and the favorable effect of positive quickening on the output of the man-machine system. Damping the motion of the indicator needle also improved performance. The optimum combination appears to be the quickening produced by 5© of gyro tilt plus 500% of normal damping. The findings are discussed in relation to a simplified model of the experimental man-machine system."--Abstract.
Author: 
Author: Defense Documentation Center (U.S.)
Author: 
Author: Lavon E. Trygg
Author: Aerospace Medical Research Laboratories (U.S.). Behavioral Sciences Laboratory
Author: 
Author: Aerospace Research Laboratories (U.S.). Behavioral Sciences Laboratory
Author: United States. 6570th Aerospace Medical Research Laboratories. Behavioral Sciences Laboratories
Author: Rebecca Jane Green