Robust adaptive flight-path reconstruction technique for nonsteady longitudinal flight test maneuvers-Reference-Cited by-同舟云学术

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Robust adaptive flight-path reconstruction technique for nonsteady longitudinal flight test maneuvers

Published:1988-01 Issue:1 Volume:11 Page:72-79
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Verhaegen M. H.¹

Affiliation:

1. NASA Ames Research Center, Moffett Field, California

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/10.2514/3.20272

Reference19 articles.

1. Quasi-Linearizatioh Technique for Estimating Aircraft States from Flight Data

2. 4Mulder, J: A; "Design and Evaluation of Dynamic Flight Test Manoeuvres," Ph.D. Dissertation,Dept. of Aeronautical Engineering, Delft University of technology, Delft, the Netherlands,Oct. 1986.

3. 5Etkin, B.,Dynamics of Atmospheric Flight, Wiley, New York, 1975.

Cited by 2 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. Study on the Method of Identifying Aircraft Parameters Based on Thrust Coupling;Journal of Physics: Conference Series;2023-04-01

2. Robust flight reconstruction for helicopter simulation and training;Journal of Aircraft;1992-05

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