Stability analysis for inverse simulation of aircraft

Aeronautical Journal

Volumn 102, Issue 1016, 1998, Pages 345-350

  Yip, K M ^a   Leng, G ^a  

^a NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; INVARIANCE; INVERSE PROBLEMS; LINEAR CONTROL SYSTEMS; MANEUVERABILITY; MATHEMATICAL MODELS; SYSTEM STABILITY;

AIRCRAFT INVERSE SIMULATION; NEWTON'S METHOD;

FLIGHT SIMULATORS;

EID: 0032092159     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (12)

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4. HESS, R.A., GAO, C. and WANG, S.H. General technique for inverse simulation applied to aircraft manoeuvres, J Guid, Com and Dynam, 1991, 14, (5), pp 920-926.
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9. RUTHERFORD, S. and THOMSON, D.G. Improved methodology for inverse simulation, Aeronaut J, March 1996, 100, (993) pp 79-86.
10. MATTEIS, G., Socio, L. and LEONESSA, A. Solution of aircraft inverse problem by local optimisation, J Guid, Cont and Dynam, 1995, 18, (3), pp 567-571.
11. LEE, S. and KIM, Y. Time-domain finite element method for inverse problem of aircraft manoeuvres, J Guid, Cont and Dynam, 1997, 20, (1), pp 97-103.
12. GREENSPAN, D. and CASULLI, V. Numerical Analysis for Applied Mathematics, Science, and Engineering, Addison-Wesley Publishing, 1988, pp 23-35.