Výsledky vyhledávání - "Kenny K. Cheung"

Development and Evaluation of a Full Flight Envelope Integrated Flight and Vibration Controller

Autor: Kenny K. Cheung, Marc D. Takahashi, Mark J. S. Lopez, J. V. R. Prasad, Mark B. Tischler

Publikováno v: Journal of the American Helicopter Society. 64:1-11

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1eb0fe310b259e8a3d6b0be975bcfd37
https://doi.org/10.4050/jahs.64.012001

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Development and Simulation of Damage Tolerant Control Laws for a Compound Helicopter

Autor: Christina M. Ivler, Joseph A. Wagster, Joseph F. Horn, Derek O. Bridges, Mark B. Tischler, Eric N. Johnson, Mark J. S. Lopez, Kenny K. Cheung, Marit E. Knapp

Publikováno v: AIAA Scitech 2020 Forum.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7270ae2f9a7e1266d3150097ccb5ffd5
https://doi.org/10.2514/6.2020-1831

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System Identification and Controller Optimization of Coaxial Quadrotor UAV in Hover

Autor: Frank C. Sanders, Kenny K. Cheung, Subodh Bhandari, Mark B. Tischler, Sung H. Cho

Publikováno v: AIAA Scitech 2019 Forum.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::0a3751651e30dfab81212c600865a3b8
https://doi.org/10.2514/6.2019-1075

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Practical Methods for Aircraft and Rotorcraft Flight Control Design: An Optimization-Based Approach

Autor: Mark B. Tischler, Tom Berger, Christina M. Ivler, Mohammadreza H. Mansur, Kenny K. Cheung, Jonathan Y. Soong

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::fef728fdb5afef9c9f708b1f2353bdb3
https://doi.org/10.2514/4.104435

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Discrete Time Finite Element Transfer Matrix Method Development for Modeling and Decentralized Control

Autor: Kenny K. Cheung, Nick B. Cramer, Mircea Teodorescu, Sean Shan-Min Swei

Publikováno v: Volume 8: 27th Conference on Mechanical Vibration and Noise.

The current emphasis on increasing aeronautical efficiency is leading the way to a new class of lighter more flexible airplane materials and structures, which unfortunately can result in aeroelastic instabilities. To effectively control the wings def

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::40ccf925f32f630c4b4539ab4096b3f6
https://doi.org/10.1115/detc2015-47812

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Modernized Control Laws for UH-60 BLACK HAWK Optimization and Flight-Test Results

Autor: Kenny K. Cheung, Sean Shan-Min Swei, Christopher L. Blanken, Alexander Faynberg, Mark B. Tischler, Vineet Sahasrabudhe

Publikováno v: Journal of Guidance, Control, and Dynamics. 28:964-978

Modernized control laws were developed to provide an attitude-command/attitude-hold response type for the UH-60 BLACK HAWK helicopter and thereby afford improved handling qualities for near-Earth operation in night and poor weather. The inner-loop sy

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ea37f7ca10cff0ee552c85a323727529
https://doi.org/10.2514/1.8021

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