Identification of Nonlinear Motion Perception Dynamics Using Time-Domain Pilot Modeling

被引:7
|
作者
Pool, D. M. [1 ]
Pais, A. R. Valente [1 ]
de Vroome, A. M. [1 ]
van Paassen, M. M. [1 ]
Mulder, M. [1 ]
机构
[1] Delft Univ Technol, Control & Simulat Div, Fac Aerosp Engn, NL-2600 GB Delft, Netherlands
关键词
CONTROL BEHAVIOR; DISTURBANCE-REJECTION; FLIGHT SIMULATOR; VERTICAL AXIS; ROLL-MOTION; CUES; THRESHOLDS; TASKS; PITCH;
D O I
10.2514/1.56236
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A method to estimate nonlinear dynamics in pilot manual control behavior is described, and it is applied to estimating the magnitude of vestibular thresholds from experimental tracking data. The three-step identification procedure uses time-domain manual tracking data to identify the parameters of a multimodal pilot model that includes a nonlinear absolute motion perception threshold. The procedure is evaluated using experimental data and pilot model simulations. To vary the fraction of the applied simulator motion that is below threshold and the possible effects of the vestibular threshold on the adopted control strategy, values of 0.25, 0.5.0.75, and 1 for the motion cueing gain Were evaluated. For both the experimental and simulation data, the identification method yields the most consistent and accurate results for the unity motion gain. Reliable estimates of pilot motion perception thresholds from active manual tracking data require sufficient excitation of the vestibular modality.
引用
收藏
页码:749 / 763
页数:15
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