Feedback Control of Flight Speed to Reduce Unmanned Aerial System Noise-Reference-Cited by-同舟云学术

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Feedback Control of Flight Speed to Reduce Unmanned Aerial System Noise

Published:2018-06-24 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA/CEAS Aeroacoustics Conference
language:
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Author:

Galles Matthew B.¹,Schiller Noah H.¹,Ackerman Kasey A.¹,Newman Brett A.²

Affiliation:

1. NASA Langley Research Center

2. Old Dominion University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2950

Reference14 articles.

1. NASA Langley Distributed Propulsion VTOL TiltWing Aircraft Testing, Modeling, Simulation, Control, and Flight Test Development

2. Geometric 3D Path-Following Control for a Fixed-Wing UAV on SO(3)

3. Xargay, E. M. “Time-Critical Cooperative Path-Following Control of Multiple Unmanned Aerial Vehicles,” Ph.D. thesis,University of Illinoisat Urbana-Champaign,2013.

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. Challenges and opportunities for low noise electric aircraft;International Journal of Aeroacoustics;2022-06-28

2. Tonal Noise Prediction of a Distributed Propulsion Unmanned Aerial Vehicle;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

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