Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

Online ISSN 1552-4485; Print ISSN 0033-569X

   
 

 

System identification and prediction--An algorithm using a Newtonian iteration procedure


Author: Theodore R. Goodman
Journal: Quart. Appl. Math. 24 (1966), 249-255
DOI: https://doi.org/10.1090/qam/99918
MathSciNet review: QAM99918
Full-text PDF Free Access

Abstract | References | Additional Information

Abstract: A mathematical technique, especially suitable for programming on a high speed digital computer, is presented for identifying a complete dynamic system having unknown parameters when data concerning one variable of the system is available.


References [Enhancements On Off] (What's this?)

  • [1] James J. Donegan, Samuel W. Robinson, Jr., and Ordway B. Gates, Jr., Determination of lateral-stability derivatives and transfer-function coefficients from frequency response data for lateral motions, NASA TN 3083, May 1954.
  • [2] W. W. Huff, Jr., Application of dynamic testing procedures to stability and control flight test program, NATO Report 191, April 1958.
  • [3] W. O. Breuhaus, Resume of the time vector method as a means for analyzing aircraft stability problems, WADC TR 52-299, November 1962.
  • [4] Marvin Shinbrot, A least squares curve fitting method with applications to the calculation of stability coefficients from transient-response data, Tech. Notes Nat. Adv. Comm. Aeronaut., 1951 (1951), no. 2341, 52. MR 0042809
  • [5] Harry Greenberg, A survey of methods for determining stability parameters of an airplane from dynamic flight measurements, NACA TN 2340, April 1951.
  • [6] Roxanah B. Yancey, Herman A. Rediess, and Glen H. Robinson, Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for Mach number 0.6 to 3.4, NASA TN D-1060, January 1962.
  • [7] Johnny M. Rampy, Donald T. Berry, Determination of stability derivatives from flight test data by means of operation analog matching, 11th Annual Air Force Science and Engineering Symposium, October 1964.
  • [8] Franklin F. Eckhart and Robert P. Harper, Jr., Analysis of longitudinal responses of unstable aircraft, Cornell Aero Lab Report BA-1610-F-1, September 1964.
  • [9] S. J. Kahne, Orbit determination using arbitrarily spaced data, Proc. First Allerton Conf. on Circuit and System Theory, University of Illinois, Urbana, Ill. 1963.
  • [10] S. J. Kahne, Note on two-point boundary value problems, Trans. IEEE, AC-8, 257, 1963.
  • [11] K. S. Prasanna Kumar and R. Sridhar, On the identification of control systems by the quasi-linearization method, IEEE Trans. Automatic Control AC-9 (1964), 151–154. MR 0180426
  • [12] R. Bellman, H. Kagiwada, and R. Kalaba, Quasilinearization, system identification, and prediction, Rand Corporation Memorandum RN 3812-PR, August 1963.


Additional Information

DOI: https://doi.org/10.1090/qam/99918
Article copyright: © Copyright 1966 American Mathematical Society


Brown University The Quarterly of Applied Mathematics
is distributed by the American Mathematical Society
for Brown University
Online ISSN 1552-4485; Print ISSN 0033-569X
© 2017 Brown University
Comments: qam-query@ams.org
AMS Website