1970
DOI: 10.1109/tmms.1970.299992
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Investigation of Motion Requirements in Compensatory Control Tasks

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Cited by 14 publications
(7 citation statements)
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“…In corroboration of the aircraft-oriented findings of Young (1967) and Bergeron (1970), the results of this research clearly support the thesis that moving-base simulation is superior to fixed-base simulation with respect to operator performance. Performance measures of yaw deviation and lateral deviation demonstrated significant decreases with the collective addition of roll, yaw, and lateral translation cues to an otherwise fixed-base simulator.…”
Section: Audio Cue Influencesupporting
confidence: 81%
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“…In corroboration of the aircraft-oriented findings of Young (1967) and Bergeron (1970), the results of this research clearly support the thesis that moving-base simulation is superior to fixed-base simulation with respect to operator performance. Performance measures of yaw deviation and lateral deviation demonstrated significant decreases with the collective addition of roll, yaw, and lateral translation cues to an otherwise fixed-base simulator.…”
Section: Audio Cue Influencesupporting
confidence: 81%
“…For most applications, the simulation of angular motions was shown to be more beneficial than were the translational motion cues. Bergeron (1970) conducted experiments with a two-axis simulator in which compensatory tracking tasks were performed. Although no significant differences were observed in the single-axis tests, the two-axis motion tests (pitch and yaw, and pitch and roll) showed significant differences in the tracking errors for the motion/ no motion comparison.…”
Section: Literature Reviewmentioning
confidence: 99%
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“…1(b), the HC utilizes a combination of at least two of the following control strategies: 1) a feedforward response (H pt ) on the target f t [101], [102], 2) a compensatory feedback response (H pe ) on the error e as in compensatory tracking [101], and 3) a feedback response (H px ) on the system output x [101]- [103]. The theoretically optimal pure feedforward control law approximates the inverse system dynamics, i.e., H pt ≈ 1/H c [101], [104], while feedback of the system output x is useful for mechanizing a stabilizing "inner" control loop, mostly for tasks with sluggish system dynamics [101].…”
Section: Pursuit Trackingmentioning
confidence: 99%
“…Data have been collected from a number of investigations performed at Delft University of Technology 7,[9][10][11][12] and from a number of studies found in literature. 4,8,[13][14][15] This paper will provide a short overview of the scope and setup of all these different experiments. The main objective of this paper, however, is to use the total set of collected data to identify consistent trends in typical dependent measures of pilot control strategy and the parameters that define the applied motion cueing setting.…”
Section: Introductionmentioning
confidence: 99%