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60.
Bray, R. S.: A Study of Vertical Motion Requirements for Landing Simulation. Human Factors, vol. 15, no. 6, 1973, pp. 561–568.
61.
Hess, R. A.; and Malsbury, T.: Closed-Loop Assessment of Flight Simulator Fidelity. AIAA
J. Guidance, Control, and Dynamics, vol. 14, no. 1, 1991, pp. 191–197.
62.
Snedecor, G. W.; and Cochran, W. G.: Statistical Methods, Sixth Ed., The Iowa State University Press. Ames, Iowa, 1967, p. 265.
63.
Paulk, C. H., Jr.; Astill, D. L.; and Donley, S. T.: Simulation and Evaluation of the SH-2F Helicopter in a Shipboard Environment Using the Interchange-able Cab System. NASA TM-84387, 1983.
64.
Ferguson, S. W.; Clement, W. F.; Cleveland, W. B.; and Key, D. L.: Assessment of Simulation Fidelity Using Measurements of Piloting Technique in Flight. Proceedings of the American Helicopter Society, May 1984, pp. 67–92.
65.
Johnson, W. W.; and Schroeder, J. A.: Visual-Motion Cueing in the Control of Altitude. IEEE International Conference on Systems, Man, and Cybernetics, Vancouver, British Columbia, Oct. 1995, pp. 2676–2681.
66.
Warren, R.: Optical Transformation during Movement: Review of the Optical Concomitants of Egomotion. Report No. AFOSR-TR-82-1028, Aviation Psychology Laboratory, Ohio State University, Columbus, Ohio, Oct. 1982.
67.
Johnson, W. W.; and Awe, C. A.: The Selective Use of Functional Optical Variables in the Control of Forward Speed. NASA TM-108849, 1994.
68.
Grant, P. R.; and Reid, L. D.: Motion Washout Filter Tuning: Rules and Requirements. AIAA J. Aircraft, vol. 34, no. 2, Mar.–Apr. 1997, pp. 145–151.
69.
Grant, P. R.; and Reid, L. D.: PROTEST: An Expert System for Tuning Simulator Washout Filters. AIAA J. Aircraft, vol. 34, no. 2, Mar.–Apr. 1997, pp. 152–159.
70.
Hess, R. A.: Model for Human Use of Motion Cues in Vehicular Control. AIAA J. Guidance, Control, and Dynamics, vol. 13, no. 3, 1990, pp. 476–482.
71.
Hess, R. A.: Theory for Aircraft Handling Qualities Based upon a Structural Pilot Model. AIAA J. Guidance, Control, and Dynamics, vol. 12, no. 6, 1989, pp. 792–797.
72.
Breuhaus, W. O.: Recent Experience with In-Flight Simulation., AGARD CP-17, pt. 2, Sept. 1966, pp. 577–620.
73.
Heffley, R. K.; Clement, W. F.; et al.: Determina-tion of Motion and Visual System Requirements for Flight Training Simulators. Technical Report 546,
U. S. Army Research Institute for the Behavioral and Social Sciences, Fort Rucker, Ala., Aug. 1981.
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