In-flight system identification

23rd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1998, Pages 238-247

  Morelli, Eugene A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DATA HANDLING; FREQUENCY DOMAIN ANALYSIS; INFORMATION ANALYSIS; ITERATIVE METHODS; RELIGIOUS BUILDINGS; TESTING;

ACCURATE MODELING; COMPUTATIONAL REQUIREMENTS; DYNAMIC CHARACTERISTICS; EXPERIMENT DESIGN; FREQUENCY DOMAINS; IMMEDIATE FEEDBACKS; REAL TIME DATA ANALYSIS; SIMULATION EXAMPLE;

FLIGHT SIMULATORS;

EID: 84983127188     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4261     Document Type: Conference Paper

References (10)

1. Gelb, A., et al. Applied Optimal Estimation, The M. I. T. Press, Cambridge, MA. 1974.
2. Garcia-Velo, J. and Walker, B. K. "Aerodynamic Parameter Estimation for High-Performance Aircraft Using Extended Kalman Filtering," Journal of Guidance, Control and Dynamics, Vol. 20, No. 6, November-December 1997. pp. 1257-9.
3. Kokolios, A. "Use of a Kalman Filter for the Determination of Aircraft Aerodynamic Characteristics from Flight Test Data," AIAA Paper 94-0010, 32nd Aerospace Sciences Meeting & Exhibit. Reno, NV. January 1994.
4. Bauer, J. E. and Andrisani, D. "Estimating Short-Period Dynamics using an Extended Kalman Filter," AIAA Paper AIAA-90-1277-CP, Fifth Biannual Flight Test Conference. Ontario, CA. May 1990.
5. Kaufman, H. "Aircraft Parameter Identification Using Kalman Filtering," Proceedings of the National Electronics Conference, Vol. XXV, pp. 85-9. December 1969.
6. Stevens, B. L. and Lewis, F. L. Aircraft Control and Simulation, John Wiley & Sons, Inc. New York, NY. 1992.
7. Morelli, E. A. "High Accuracy Evaluation of the Finite Fourier Transform Using Sampled Data," NASA TM 110340, June 1997.
8. Klein, V. "Aircraft Parameter Estimation in Frequency Domain," AIAA paper 78-1344, Atmospheric Flight Mechanics Conference, Palo Alto, CA, August 1978.
9. Morelli, E. A. "Flight Test Validation of Optimal Input Design and Comparison to Conventional Inputs," AIAA paper 97-3711, AIAA Atmospheric Flight Mechanics Conference. New Orleans, LA. August 1997.
10. Mehra, R. K. and Gupta, N. K. "Status of Input Design for Aircraft Parameter Identification," AGARD-CP-172, paper 12. May 1975.