Modified recursive maximum likelihood adaptive filter for nonlinear aircraft flight-path reconstruction-Reference-Cited by-同舟云学术

Modified recursive maximum likelihood adaptive filter for nonlinear aircraft flight-path reconstruction

Published:1996-11 Issue:6 Volume:19 Page:1285-1295
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Chu Q. P.¹,Mulder J. A.¹,van Woerkom P. T. L. M.¹

Affiliation:

1. Delft University of Technology, 2629 HS Delft, The Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.21784

Reference33 articles.

1. 3Mulder, J. A. "Design and Evaluation of Dynamic Flight Test Manoeuvres," Ph.D. Thesis, Faculty of Aerospace Engineering,Delft Univ. of Technology, Delft,The Netherlands, Oct. 1986.

2. Jonkers, H. K. "Application of the Kalman Filter to Flight Path Reconstruction from Flight Test Data Including Estimation of Instrumental Bias Error Corrections" Ph.D. Thesis, Faculty of Aerospace Engineering,Delft Univ. of Technology, Delft,The Netherlands, Feb. 1976.

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