TY - GEN
T1 - Correlation techniques in robust nonlinear system realization/identification
AU - Stry, Greselda I.
AU - Mook, D. Joseph
PY - 1991
Y1 - 1991
N2 - The fundamental challenge in identification of nonlinear dynamic systems is determining the appropriate form of the model. A robust technique is presented in this paper which essentially eliminates this problem for many applications. The technique is based on the Minimum Model Error (MME) optimal estimation approach. A detailed literature review is included in which fundamental differences between the current approach and previous work is described. The most significant feature of the current work is the ability to identify nonlinear dynamic systems without prior assumptions regarding the form of the nonlinearities, in contrast to existing nonlinear identification approaches which usually require detailed assumptions of the nonlinearities. Model form is determined via statistical correlation of the MME optimal state estimates with the MME optimal model error estimates. The example illustrations indicate that the method is robust with respect to prior ignorance of the model, and with respect to measurement noise, measurement frequency, and measurement record length.
AB - The fundamental challenge in identification of nonlinear dynamic systems is determining the appropriate form of the model. A robust technique is presented in this paper which essentially eliminates this problem for many applications. The technique is based on the Minimum Model Error (MME) optimal estimation approach. A detailed literature review is included in which fundamental differences between the current approach and previous work is described. The most significant feature of the current work is the ability to identify nonlinear dynamic systems without prior assumptions regarding the form of the nonlinearities, in contrast to existing nonlinear identification approaches which usually require detailed assumptions of the nonlinearities. Model form is determined via statistical correlation of the MME optimal state estimates with the MME optimal model error estimates. The example illustrations indicate that the method is robust with respect to prior ignorance of the model, and with respect to measurement noise, measurement frequency, and measurement record length.
UR - https://www.scopus.com/pages/publications/0025814296
M3 - Conference contribution
AN - SCOPUS:0025814296
SN - 0877033390
T3 - Advances in the Astronautical Sciences
SP - 453
EP - 469
BT - Advances in the Astronautical Sciences
T2 - Proceedings of the AAS/AIAA Spaceflight Mechanics Meeting Part 1 (of 2)
Y2 - 11 February 1991 through 13 February 1991
ER -