Flight clearance analysis using global nonlinear optimisation-based search algorithms

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Forssell, Lars S ^a  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT SYSTEMS; ANALYSIS TECHNIQUES; FLIGHT CLEARANCE; MODEL UNCERTAINTIES; NON-LINEAR AIRCRAFT MODELS; PARAMETRIC MODELING; SEARCH ALGORITHMS; SEARCH TECHNIQUE;

AIRCRAFT MODELS; RELIABILITY ANALYSIS; UNCERTAINTY ANALYSIS;

OPTIMIZATION;

EID: 84896806938     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. C. Fielding, A. Varga, S. Bennani and M. Selier Advanced Techniques for Clearance of Flight Control Laws. Springer Verlag, 2002
2. Military Standard Flying Qualities of Piloted Aircraft. MIL-SPEC-1797A.
3. GARTEUR FM(EG17). Terms of Reference for GARTEUR Flight Mechanics Action Group FM(AG11) on: New Analysis Techniques for Clearance of Flight Control Laws. FM(EG17)M1-v1, 19 February 1999.
4. L. Forssell and A. Sandblom. Optimisation- Based Non-linear Analysis of the HIRM model. GARTEUR/TP-119-19, 2002
5. A. Varga Robust stability and performance analysis of flight control laws using optimization-based worst-case search: Linear stability criteria. GARTEUR/TP-119-15
6. F. Karlsson, U. Korte and S. Scala. Selected Criteria for Clearance of the HIRM- plus Flight Control Laws,GARTEUR/TP- 119-2-A1(addendum to GARTEUR/TP-119- 2). GARTEUR FM(AG11), Nov. 1999.
7. D. Moormann and D. Bennett. The HIRM- plus Aircraft Model and Control Laws Development. GARTEUR/TP-119-2, 1999.
8. The MathWorks Inc. Optimization Toolbox Users Guide December, 1996.
9. R. Houck, J. Jones and M. Kay. A Genetic Algorithm for Function Optimization: A Matlab Implementation. North Carolina State University, 1995.
10. W. Huyer and A. Neumaier. Global Optimization by Multilevel Co-ordinate Search. Kluver Academic Publishers, 1998.
11. L. Forssell and A. Hyden Optimisation Based Worst Case Search of ADMIRE, GARTEUR/TP-119-26, 2002
12. A. Varga, et.al. Post-Design Stability Robustness Assessment of the RCAM Controller Design Entries, GARTEUR/TP-088-35, 1997.
13. L. Forssell Aero-Data Model in a Research Environment (ADMIRE) for Flight Control Robustness Evaluation, GARTEUR FM(AG11)/TP-119-7-v2, 2001.
14. H. Luijerink Baseline Flight Clearance Solution of ADMIRE 3.4f, GARTEUR FM(AG11)/TP-119-18-v2, 2001.
15. L. Ingber Adaptive Simulated Annealing (ASA), http://www.ingber.com, 1993.