Zobrazeno 1 - 10 of 46 pro vyhledávání: '"John J. Burken"'
2
Flight Control with Optimal Control Allocation Incorporating Structural Load Feedback
Autor: Brian R. Taylor, Christine V. Jutte, John J. Burken, Khanh V. Trinh, Susan A. Frost, Marc Bodson
Publikováno v: Journal of Aerospace Information Systems. 12:825-834
Advances in sensors and avionics computation power suggest real-time structural load measurements could be used in flight control systems for improved safety and performance. A conventional transport flight control system determines the moments neces
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::45e476fbef9625fb0e3dd65db4a91202
https://doi.org/10.2514/1.i010278
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4
Takagi-Sugeno Fuzzy Model-Based Flight Control and Failure Stabilization
Autor: Evan J. Butler, Hua O. Wang, John J. Burken
Publikováno v: Journal of Guidance, Control, and Dynamics. 34:1543-1555
This paper presents a Takagi–Sugeno fuzzy model-based approach to modeling, controlling, and stabilizing an aircraft in both normal and damaged conditions. The major contributions of this paper are as follows. First, it introduces the Takagi–Suge
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d34841d453091af7436d221367f78271
https://doi.org/10.2514/1.52509
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5
Self-Organizing Radial Basis Function Networks for Adaptive Flight Control
Autor: Rama K. Yedavalli, John J. Burken, Praveen Shankar
Publikováno v: Journal of Guidance, Control, and Dynamics. 34:783-794
The performance of nonlinear flight-control algorithms, such as feedback linearization and dynamic inversion, is heavily dependent on the fidelity of the dynamic model being inverted. Incomplete or incorrect knowledge of the aircraft dynamics results
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::8345ac71a6a68f39fb5ae0f815eac45f
https://doi.org/10.2514/1.51135
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6
Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation
Autor: John J. Burken, Zhenglu Wu, Ping Lu, Cathy Bahm
Publikováno v: Journal of Guidance, Control, and Dynamics. 24:482-493
Two methods for control system reconfiguration have been investigated. The first method is a robust servomechanism control approach (optimal tracking problem) that is a generalization of the classical proportional-plus-integral control to multiple in
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5ec28562a7c56749560305124e9c73be
https://doi.org/10.2514/2.4769
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8
Flight-Test Results of Propulsion-Only Emergency Control System on MD-11 Airplane
Autor: John J. Burken, Frank W. Burcham
Publikováno v: Journal of Guidance, Control, and Dynamics. 20:980-987
A large, civilian, multiengine transport MD-11 airplane control system was recently modie ed to perform as an emergency backup controller using engine thrust only. The emergency backup system, referred to as the propulsion-controlled aircraft (PCA)sy
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f5dab7a44ee29e5aa9a64d2c7e739f40
https://doi.org/10.2514/2.4143
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9
X-29 flight control system: lessons learned
Autor: Jeffrey E. Bauer, John J. Burken, John T. Bosworth, Robert Clarke
Publikováno v: International Journal of Control. 59:199-219
Two X-29A aircraft were flown at the NASA Dryden Flight Research Facility over a period of eight years. The airplanes' unique features are the forward-swept wing, variable incidence close-coupled canard and highly relaxed longitudinal static stabilit
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5a3810976864f97c880126ad143d15dd
https://doi.org/10.1080/00207179408923075
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10
Linear Quadratic Tracking Design for a Generic Transport Aircraft with Structural Load Constraints
Autor: Susan A. Frost, Brian R. Taylor, John J. Burken
Publikováno v: AIAA Guidance, Navigation, and Control Conference.
When designing control laws for systems with constraints on the tracking performance, control allocation methods can be utilized. Control allocation methods are used when there are more command inputs than controlled variables. Control allocators can
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::43de704c9afdb102e2d172f342231c71
https://doi.org/10.2514/6.2011-6304
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