Uses of parameter estimation in flight test-Reference-Cited by-同舟云学术

Uses of parameter estimation in flight test

Published:1983-12 Issue:12 Volume:20 Page:1043-1049
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Iliff Kenneth W.¹,Maine Richard E.¹

Affiliation:

1. NASA Ames Research Center, Edwards, California

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.48210

Reference14 articles.

1. ^aine, R.E. and Iliff, K.W. "User's Manual for MMLE3, a General FORTRAN Program for Maximum Likelihood Parameter Estimation," NASA TP-1563,1980.

2. 2Iliff, K.W. and Maine, R.E. "Practical Aspects of Using a Maximum Likelihood Estimation Method to Extract Stability and Control Derivatives From Flight Data," NASA TN D-8209,1976.

3. 3Iliff, K.W., Maine, R.E., and Montgomery, T.D. "Important Factors in the Maximum Likelihood Analysis of Flight Test Maneuvers," NASA TP-1459,1979.

4. Application of high-alpha control system concepts to a variable-sweep fighter airplane

5. Flight test experience with high-alpha control system techniques on the F-14 airplane

Cited by 4 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. Frequency Response Estimation for Multiple Aircraft Control Loops Using Orthogonal Phase-Optimized Multisine Inputs;Processes;2022-03-22

2. A Collection of Modern Resources for Education in Atmospheric Flight Mechanics;AIAA SCITECH 2022 Forum;2022-01-03

3. Aircraft System Identification;Aircraft Aerodynamic Parameter Estimation from Flight Data Using Neural Partial Differentiation;2021

4. Parameter Uncertainty for Aircraft Aerodynamic Modeling using Recursive Least Squares;AIAA Atmospheric Flight Mechanics Conference;2016-01-01