Robust Stall Spin Flight Path Control with Flight Test Validation-Reference-Cited by-同舟云学术

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Robust Stall Spin Flight Path Control with Flight Test Validation

Published:2023-03 Issue:3 Volume:46 Page:553-559
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Hopwood Jeremy W.¹^ORCID,Gresham James L.¹,Woolsey Craig A.¹^ORCID

Affiliation:

1. Virginia Tech, Blacksburg, Virginia 24061

Funder

Ames Research Center

Center for Unmanned Aircraft Systems, National Science Foundation

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

https://arc.aiaa.org/doi/pdf/10.2514/1.G007016

Reference16 articles.

1. KinzigB. “Global Hawk Systems Engineering Case Study,” Air Force Center for Systems Engineering, Air Force Institute of Technology, Doc. 31, 2009, https://scholar.afit.edu/docs/31.

2. AirSTAR Beyond Visual Range System Description and Preliminary Test Results

3. “2020-21 Design, Build, Fly Rules,” AIAA, 2020, https://www.aiaa.org/dbf/competition-information/rules-resources.

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. Flight-Test System Identification Techniques and Applications for Small, Low-Cost, Fixed-Wing Aircraft;Journal of Aircraft;2023-09

2. Spin Aerodynamic Modeling for a Fixed-Wing Aircraft Using Flight Data;Journal of Aircraft;2023-08-25

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