Reduced Order Guidance Methods and Probabilistic Techniques in Addressing Mission Uncertainty

Presented at the 6th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, September 4-6, 1996.

[1]  P. Wirsching,et al.  Advanced Reliability Methods for Structural Evaluation , 1987 .

[2]  Derek J. Pike,et al.  Empirical Model‐building and Response Surfaces. , 1988 .

[3]  A. J. Calise,et al.  Singular Perturbations in Flight Mechanics , 1994 .

[4]  Daniel P. Schrage,et al.  Effect of Mission Requirements on the Economic Robustness of an HSCT Concept , 1997 .

[5]  Dimitri N. Mavris,et al.  Application of Probabilistic Methods for the Determination of an Economically Robust HSCT Configuration , 1996 .

[6]  Sidney Addelman,et al.  trans-Dimethanolbis(1,1,1-trifluoro-5,5-dimethylhexane-2,4-dionato)zinc(II) , 2008, Acta crystallographica. Section E, Structure reports online.

[7]  Maciejowsk Multivariable Feedback Design , 1989 .

[8]  Robert F. Stengel,et al.  Stochastic measures of performance robustness in aircraft control systems , 1992 .

[9]  Anthony J. Calise,et al.  Extended Energy Management Methods for Flight Performance Optimization , 1975 .

[10]  W. G.,et al.  THE COMPROMISE DECISION SUPPORT PROBLEM IN DEVELOPING A GENERAL ROBUST DESIGN PROCEDURE , 2022 .

[11]  Margaret J. Robertson,et al.  Design and Analysis of Experiments , 2006, Handbook of statistics.

[12]  R. L. Schultz,et al.  Aircraft performance optimization. , 1972 .

[13]  Anthony J. Calise,et al.  Singular perturbation analysis of optimal flight profiles for transport aircraft , 1977 .

[14]  George E. P. Box,et al.  Empirical Model‐Building and Response Surfaces , 1988 .

[15]  Arthur E. Bryson,et al.  Energy-state approximation in performance optimization of supersonic aircraft , 1969 .