Flight control design for a nonlinear non-minimum phase VTOL aircraft via two-step linearization

Proceedings of the 40th IEEE Conference on Decision and Control (Cat. No.01CH37228) ◽

10.1109/cdc.2001.980101 ◽

2003 ◽

Cited By ~ 17

Author(s):

M. Saeki ◽

Y. Sakaue

Keyword(s):

Flight Control ◽

Control Design ◽

Minimum Phase ◽

Vtol Aircraft

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Dynamic Inversion Flight Control Design for Aircraft with Non-Minimum Phase Response

10.4271/2011-01-2617 ◽

2011 ◽

Cited By ~ 2

Author(s):

Howard P. Lee ◽

Joshua W. Clemens ◽

Hussein M. Youssef

Keyword(s):

Flight Control ◽

Control Design ◽

Phase Response ◽

Dynamic Inversion ◽

Minimum Phase

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121 Nonlinear Control Design of a VTOL Aircraft with Non-minimum Phase Property

The Proceedings of the Symposium on the Motion and Vibration Control ◽

10.1299/jsmemovic.2001.7.80 ◽

2001 ◽

Vol 2001.7 (0) ◽

pp. 80-83

Author(s):

Masami SAEKI ◽

Yoshinobu SAKAUE

Keyword(s):

Nonlinear Control ◽

Control Design ◽

Minimum Phase ◽

Phase Property ◽

Vtol Aircraft

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Launcher flight control design using robust wind disturbance observation

Acta Astronautica ◽

10.1016/j.actaastro.2021.05.044 ◽

2021 ◽

Author(s):

Pedro Simplício ◽

Andrés Marcos ◽

Samir Bennani

Keyword(s):

Flight Control ◽

Control Design ◽

Wind Disturbance

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Fault tolerant linear parameter varying flight control design, verification and validation

Journal of the Franklin Institute ◽

10.1016/j.jfranklin.2021.02.040 ◽

2021 ◽

Author(s):

Andrés Marcos ◽

Sérgio Waitman ◽

Masayuki Sato

Keyword(s):

Flight Control ◽

Fault Tolerant ◽

Control Design ◽

Verification And Validation ◽

Design Verification ◽

Linear Parameter ◽

Linear Parameter Varying ◽

Parameter Varying

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On data-driven control design for non-minimum-phase plants: A comparative view

2016 IEEE 55th Conference on Decision and Control (CDC) ◽

10.1109/cdc.2016.7799373 ◽

2016 ◽

Cited By ~ 2

Author(s):

Gianmarco Rallo ◽

Simone Formentin ◽

Sergio M. Savaresi

Keyword(s):

Control Design ◽

Data Driven ◽

Minimum Phase

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Output feedback based adaptive composite nonlinear flight control design for a small-scale un-crewed helicopter

ISA Transactions ◽

10.1016/j.isatra.2021.08.004 ◽

2021 ◽

Author(s):

Femi Thomas ◽

Mija S.J.

Keyword(s):

Flight Control ◽

Output Feedback ◽

Control Design ◽

Small Scale ◽

Adaptive Composite

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Robust flight control design for the HIRM via linear quadratic methods

10.2514/6.1998-4244 ◽

1998 ◽

Cited By ~ 1

Author(s):

F. Amato ◽

M. Mattei ◽

S. Scala ◽

L. Verde

Keyword(s):

Flight Control ◽

Control Design ◽

Linear Quadratic ◽

Robust Flight Control

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Quadratic Stabilization With Partial Eigenstructure Assignment: Application To Flight Control Design

IFAC Proceedings Volumes ◽

10.1016/s1474-6670(17)40724-5 ◽

2001 ◽

Vol 34 (15) ◽

pp. 179-184 ◽

Cited By ~ 2

Author(s):

Atsushi Satoh ◽

Kenji Sugimoto

Keyword(s):

Flight Control ◽

Control Design ◽

Eigenstructure Assignment ◽

Quadratic Stabilization

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Passive Fault-Tolerant Flight Control Design Example for Elevator Efficiency Reduction Using Structured H∞ Control*

10.1109/med51440.2021.9480174 ◽

2021 ◽

Author(s):

Masayuki Sato

Keyword(s):

Flight Control ◽

Fault Tolerant ◽

Control Design

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Uncertainty Modeling, Analysis and Robust Flight Control Design for a Small UAV System

AIAA Guidance, Navigation and Control Conference and Exhibit ◽

10.2514/6.2008-7434 ◽

2008 ◽

Cited By ~ 10

Author(s):

Yew Chai Paw ◽

Gary Balas

Keyword(s):

Flight Control ◽

Control Design ◽

Uncertainty Modeling ◽

Modeling Analysis ◽

Small Uav ◽

Robust Flight Control

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