D-Optimal Simultaneous Multistep Excitations for Aircraft Parameter Estimation-Reference-Cited by-同舟云学术

D-Optimal Simultaneous Multistep Excitations for Aircraft Parameter Estimation

Published:2017-03 Issue:2 Volume:54 Page:747-758
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Lichota Piotr¹,Sibilski Krzysztof¹,Ohme Per²

Affiliation:

1. Warsaw University of Technology, 00-665 Warsaw, Poland

2. DLR, German Aerospace Center, 38-108 Braunschweig, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033794

Reference42 articles.

1. MarchandM. “Untersuchung der Bestimmbarkeit von Flugzeugderivativen aus Flugversuchen, ” DFVLR-IB 154/74/32, Dec. 1974.

2. KoehlerR.KnutW. “Auslegung von Eingangssignalen für die Kennwertermittlung,” DFVLR-IB 154-77/40, Dec. 1977.

3. PlaetschkeE.MulderJ. A.BreemanJ. H. “Results of Beaver Aircraft Parameter Estimation,” DFVLR-FB 83-10, Feb. 1983.

4. PlaetschkeE.MackieD. B. “Maximum-Likelihood Schätzung von Parametern linearer Systeme aus Flugversuchsdaten—Ein FORTRAN-Programm,” DFVLR-Mitt. 84-10, Jan. 1984.

5. Algorithms for aircraft parameter estimation accounting for process and measurement noise

Cited by 26 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Retrospective and Recent Examples of Aircraft and Rotorcraft System Identification at DLR;Journal of Aircraft;2023-09

2. Wavelet Transform-Based Aircraft System Identification;Journal of Guidance, Control, and Dynamics;2023-02

3. Wavelet-Based Identification for Spinning Projectile with Gasodynamic Control Aerodynamic Coefficients Determination;Sensors;2022-05-27

4. Lateral directional aircraft aerodynamic parameter estimation using adaptive stochastic nonlinear filter;The Aeronautical Journal;2021-11-18

5. Optimal Input Design for Aircraft Stability and Control Flight Testing;Journal of Optimization Theory and Applications;2021-10-20