Application of global sensitivity equations in multidisciplinary aircraft synthesis

Journal of Aircraft

Volumn 27, Issue 12, 1990, Pages 1002-1010

  Hajela, P ^a,c   Bloebaum, C L ^a,c   Sobieszczanski Sobieski, Jaroslaw ^b,d  

^a UNIVERSITY OF FLORIDA   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Department of Aerospace Engineering Mechanics and Engineering Science ^*  (United States)

^d Interdisciplinary Research Office ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85002709466     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.45974     Document Type: Article

References (10)

1. Sensburg, O., Fullhas, K., and Schimdinger, G., “Interdisciplinary Design of Aircraft Structures for Minimum Weight,” AIAA Paper 88-2302, April 1988.
2. Abdi, F., Ide, H., Levine, M., and Austel, L., “The Art of Spacecraft Design: A Multidisciplinary Challenge,” 2nd NASA/Air Force Symposium on Recent Advances in Multidisciplinary Analysis and Optimization, NASA CP-3031, Sept. 1988.
3. Sobieszczanski-Sobieski, J., “On the Sensitivity of Complex, Internally Coupled Systems,” AIAA Journal, Vol. 28, No. 1, 1990.
4. Sobieszczanski-Sobieski, J., Bloebaum, C. L., and Hajela, P., “Sensitivity of Control-Augmented Structure Obtained by a System Decomposition Method,” AIAA Paper 88-2205, April 1988 (to appear in the AIAA Journal).
5. Hajela, P., “Techniques in Optimum Structural Synthesis with Static and Dynamic Constraints,” Ph.D. Dissertation, Stanford Univ., Stanford, CA, June 1982.
6. Whetstone, W. D., “SPAR Structural Analysis System Reference Manual—System Level 13A,” Vol. 1, NASA CR-158970-1, 1978.
7. Peele, E. L., and Adams, W. M., Jr., “A Digital Program for Calculating the Interaction between Flexible Structures, Unsteady Aerodynamics and Active Controls,” NASA TM-80040, Jan. 1979.
8. Perkins, C. D., and Hage, R. E., Airplane Performance: Stability and Control, Wiley, New York, 1949.
9. Armstrong, E. S., “ORACLS—A System for Linear Quadratic Gaussian Control Law Design,” NASA TP-1106, 1978.
10. Smetana, F. O., Computer Assisted Analysis of Aircraft Performance Stability and Control, McGraw Hill, New York, 1984.