A Study of Vertical Motion Requirements for Landing Simulation

Author:

Bray Richard S.1

Affiliation:

1. Ames Research Center, NASA, Moffett Field, California

Abstract

Tests were conducted to determine the significance of vertical acceleration cues in the simulation of the visual approach and landing maneuver. Landing performance measures were obtained for four subject pilots operating a visual landing simulation mechanized in the Ames Height Control Test Apparatus, a device that provides up to ±40 ft. of vertical motion. Test results indicate that vertical motion cues are utilized in the landing task, and that they are particularly important in the simulation of aircraft with marginal longitudinal-handling qualities. To assure vertical motion cues of the desired fidelity in the landing task, it appears that a simulator must have excursion capabilities of at least ±20 ft.

Publisher

SAGE Publications

Subject

Behavioral Neuroscience,Applied Psychology,Human Factors and Ergonomics

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1. Refinement of Objective Motion Cueing Criteria Based on Three Flight Tasks;AIAA Modeling and Simulation Technologies Conference;2017-01-05

2. Rotorcraft Research at the NASA Vertical Motion Simulator;AIAA Atmospheric Flight Mechanics Conference;2009-06-14

3. Training Value of a Fixed-Base Flight Simulator with a Dynamic Seat;AIAA Modeling and Simulation Technologies Conference and Exhibit;2007-06-15

4. Conversion between control mechanisms in simulated flight: an ab initio quasi-transfer study;Australian Journal of Psychology;2002-01-01

5. Simulator Platform Motion Effects on Pilot-Induced Oscillation Prediction;Journal of Guidance, Control, and Dynamics;2000-05

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