Multiple input design for real-time parameter estimation in the frequency domain

A method for designing multiple inputs for real-time dynamic system identification in the frequency domain was developed and demonstrated. The designed inputs are mutually orthogonal in both the time and frequency domains, with reduced peak factors to provide good information content for relatively small amplitude excursions. The inputs are designed for selected frequency ranges, and therefore do not require a priori models. The experiment design approach was applied to identify linear dynamic models for the F-15 ACTIVE aircraft, which has multiple control effectors.

[1]  John J. Burken,et al.  Tailored Excitation for Multivariable Stability-Margin Measurement Applied to the X-31A Nonlinear Simulation , 1997 .

[2]  R. Bursey,et al.  F-15 ACTIVE A FLEXIBLE PROPULSION INTEGRATION TESTBED , 1994 .

[3]  Howard Kaufman,et al.  Assessment Study of the State of the Art in Adaptive Control and its Applications to Aircraft Control , 1998 .

[4]  A Morelli Eugene High Accuracy Evaluation of the Finite Fourier Transform Using Sampled Data , 1997 .

[5]  Frank L. Lewis,et al.  Aircraft Control and Simulation , 1992 .

[6]  Manfred R. Schroeder,et al.  Synthesis of low-peak-factor signals and binary sequences with low autocorrelation (Corresp.) , 1970, IEEE Trans. Inf. Theory.

[7]  P. L. Deal,et al.  Simulator study of stall/post-stall characteristics of a fighter airplane with relaxed longitudinal static stability. [F-16] , 1979 .

[8]  Eugene A. Morelli,et al.  Real-Time Parameter Estimation in the Frequency Domain , 1999 .

[9]  Ron J. Patton,et al.  Comparison of test signals for aircraft frequency domain identification , 1990 .

[10]  A.H. Haddad,et al.  Applied optimal estimation , 1976, Proceedings of the IEEE.

[11]  Vladislav Klein,et al.  Two biased estimation techniques in linear regression: Application to aircraft , 1988 .

[12]  V. Klein,et al.  Aircraft parameter estimation in frequency domain , 1978 .

[13]  Dominick Andrisani,et al.  Estimating short-period dynamics using an extended Kalman filter , 1990 .

[14]  John S. Orme,et al.  Flight Test Validation of a Frequency-Based System Identification Method on an F-15 Aircraft , 1995 .

[15]  Alexander Kokolios Use of a Kalman filter for the determination of aircraft aerodynamic characteristics from flight test data , 1994 .

[16]  Meir Pachter,et al.  System identification for adaptive and reconfigurable control , 1995 .

[17]  J. O. Flower,et al.  Application of Schroeder-Phased Harmonic Signals to Practical Identification , 1978 .

[18]  Eugene A. Morelli IN-FLIGHT SYSTEM IDENTIFICATION , 1998 .