Fixed order optimal pilot models

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-11

  Doman, David B ^a,b   Anderson, Mark R ^a  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPENSATION STRATEGY; FULL-ORDER MODELS; OPTIMAL CONTROL THEORY; OPTIMAL CONTROLS; PROJECTION SYNTHESIS; PROJECTION TECHNIQUES; QUADRATIC PERFORMANCE INDICES; SYNTHESIS TECHNIQUES;

CONTROL ENGINEERING;

EID: 84959083679     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-3871     Document Type: Conference Paper

References (15)

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3. Kleinman, D.L.; Baron, S.; and Levison, W. H., “An Optimal Control Model of Human Response — Part 1: Theory and Validation,” Automatica, Vol 16, no.3,1970, pp. 237-253.
4. Davidson, John B. and Schmidt, David K., “Modified Optimal Control Pilot Model for Computer-Aided Design and Analysis,” NASA-TM-4384, 1992.
5. Thompson, Peter M., “Minimum Flying Qualities, Vol. 3: Program CC's Implementation of the Human Optimal Control Model,” WRDCTR-89-3125, Jan. 1990.
6. Hess, Ronald A., “A Method for Generating Numerical Pilot Opinion Ratings Using the Optimal Pilot Model,” NASA TM X-73,101, 1976.
7. Efremov A.V., “Analysis of Reasons for PIO Tendency and Development of Criteria for its Prediction,” Moscow Aviation Institute, April 1995.
8. McRuer, D., “Human Dynamics in Man-Machine Systems,” Automatica, Vol. 16, 1980, pp.237-253.
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11. Baron, S. and Kleinman, D. et al., “Application of Optimal Control Theory to Prediction of Human Performance in a Complex Task,” Proceedings MIT/NASA Conference on Manual Control, March 1969.
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13. ∞ Standard Problem,” Systems and Control Letters, 1990, Vol 14, pp. 185-197.
14. Peterson, Lee D., “Optimal Projection Control of an Experimental Truss Structure,” Journal of Guidance, Control and Dynamics, Vol 14, No. 2, March-April 1991. pp. 241-250.
15. Neal, T. Peter and Smith, Rogers E.,: “An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes,” AFFDLTR-70-74, Vol 1, Dec. 1970.