Output error method and two step method for aerodynamic model identification

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 8, Issue , 2005, Pages 5882-5890

  Oliveira, Joao ^a,b   Chu, Q P ^a,b   Mulder, J A ^a,b,c   Balini, H M N K ^a,b   Vos, W G M ^a,b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT LONGITUDINAL DYNAMICS; NON-VISCOUS EULER EQUATIONS; OUTPUT ERROR METHODS; QUASI-STATIC ENVIRONMENTS;

ERROR ANALYSIS; FLIGHT DYNAMICS; IDENTIFICATION (CONTROL SYSTEMS); JET AIRCRAFT; MATHEMATICAL MODELS; TEST FACILITIES;

AERODYNAMICS;

EID: 29744431933     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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2. G.W. Milne, J.A. Mulder, M.W. Soijer, S. Juliana, and Hermansyah. Maximum likelihood stability & control derivative identification of a Cessna Citation II. AIAA 2001-4013, August 6-9 2001. Montreal, Canada.
3. Sridhar J.K. Breeman J.H. Mulder J.A., Chu Q.P. and Laban M. Non-linear aircraft flight path reconstruction review and new advances. Progress in Aerospace Sciences 35, pages 673-726, 1999.
4. Mulder J.A. Oliveira J., Chu Q.P. and Vos W.G.M. Developing a navigation system for aerodynamic model identification using the two-step method. EUCASS European Conference on Aerospace Sciences, Moscow, July 2005.
5. Mulder J.A. Chu Q.P. and Sridhar J.K. Decomposition of aircraftstate and parameter estimation problem. Proceedings of the 10th IFAC Symposium on System Identification, Vol. 3, Danish Automation Society, Copenhagen, Denmark, pp. 61-66., 1994.
6. Maine R. E. and Illiff K. W. Application of parameter estimation to aircraft stability and control - the output error approach. NASA RP 1168, June 1986.
7. M.W. Soijer. Data acquisition and analysis software as real-time processes. 31st Annual Symposium Society of Flight Test Engineers, 2000.
8. R.G. Brown and P.Y.C. Hwang. Introduction to Random Signals and Applied Kalman Filtering. John Wiley & Sons, 1997.
9. Laban M. On-line aircraft aerodynamic model identification. Ph.D. Thesis, Faculty of Aerospace Engineering, Delft University of Technology, Delft, The Netherlands, May 1994.
10. Mulder J.A. Design and evaluation of flight test manoeuvres. Ph.D. dissertation, Delft University of Technology, 1986.