An Effective Maximal-Length Sequence Design for System Identification of a Continuous-Time Linear Aircraft Model
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Yamanashi
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/64/4/64_T-20-33/_pdf
Reference16 articles.
1. 1) Schmidt, L. V.: Introduction to Aircraft Flight Dynamics, AIAA, Reston, 1998, pp. 333–354.
2. 2) Ljung, L.: System Identification—Theory for the User, 2nd ed., Prentice Hall, Upper Saddle River, NJ, 1999, pp. 1–567.
3. 3) Söderström, T. and Stoica, P.: System Identification, Prentice Hall, Upper Saddle River, NJ, 1989, pp. 1–352.
4. 4) Verhaegen, M. and Verdult, V.: Filtering and System Identification — A Least Square Approach —, Cambridge University Press, Cambridge, 2007, pp. 1–394.
5. 5) Overschee, P. and Moor, B.: Subspace Identification for Linear Systems, Kluwer Academic Publishers, Massachusetts, 1996, pp. 1–254.
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