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100417s2010 gw | s |||| 0|eng d |
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|a 9783642116902
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| 024 |
7 |
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|a 10.1007/978-3-642-11690-2
|2 doi
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| 040 |
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|a Sistema de Bibliotecas del Tecnológico de Costa Rica
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| 245 |
1 |
0 |
|a Fault Tolerant Flight Control :
|b A Benchmark Challenge /
|c edited by Christopher Edwards, Thomas Lombaerts, Hafid Smaili.
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| 250 |
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|a 1st ed. 2010.
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| 260 |
# |
# |
|a Berlin, Heidelberg :
|b Springer Berlin Heidelberg :
|b Imprint: Springer,
|c 2010.
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| 300 |
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|a 560 p. 174 illus. in color. :
|b online resource.
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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| 490 |
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|a Lecture Notes in Control and Information Sciences,
|v 399
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| 505 |
0 |
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|a Surviving the Improbable: Towards Resilient Aircraft Control -- Fault Tolerant Flight Control - A Survey -- Fault Detection and Diagnosis for Aeronautic and Aerospace Missions -- Real-Time Identification of Aircraft Physical Models for Fault Tolerant Flight Control -- Industrial Practices in Fault Tolerant Control -- RECOVER: The Benchmark Challenge -- RECOVER: A Benchmark for Integrated Fault Tolerant Flight Control Evaluation -- Assessment Criteria as Specifications for Reconfiguring Flight Control -- Design Methods and Benchmark Analysis -- Fault Tolerant Control Using Sliding Modes with On-Line Control Allocation -- An Adaptive Fault-Tolerant FCS for a Large Transport Aircraft -- Subspace Predictive Control Applied to Fault-Tolerant Control -- Fault-Tolerant Control through a Synthesis of Model-Predictive Control and Nonlinear Inversion -- A FTC Strategy for Safe Recovery against Trimmable Horizontal Stabilizer Failure with Guaranteed Nominal Performance -- Flight Control Reconfiguration Based on Online Physical Model Identification and Nonlinear Dynamic Inversion -- A Combined Fault Detection, Identification and Reconfiguration System Based around Optimal Control Allocation -- Detection and Isolation of Actuator/Surface Faults for a Large Transport Aircraft -- Real-Time Flight Simulator Assessment -- Real-Time Assessment and Piloted Evaluation of Fault Tolerant Flight Control Designs in the SIMONA Research Flight Simulator -- Piloted Evaluation Results of a Nonlinear Dynamic Inversion Based Controller Using Online Physical Model Identification -- Model Reference Sliding Mode FTC with SIMONA Simulator Evaluation: EL AL Flight 1862 Bijlmermeer Incident Scenario -- Conclusions -- Industrial Review -- Concluding Remarks.
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| 650 |
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0 |
|a Aerospace engineering.
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| 650 |
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0 |
|a Astronautics.
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| 650 |
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0 |
|a Electronics.
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| 650 |
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0 |
|a Microelectronics.
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| 650 |
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0 |
|a Control engineering.
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| 650 |
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0 |
|a Robotics.
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| 650 |
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0 |
|a Mechatronics.
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| 650 |
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0 |
|a System theory.
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| 650 |
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0 |
|a Automotive engineering.
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| 650 |
1 |
4 |
|a Aerospace Technology and Astronautics.
|
| 650 |
2 |
4 |
|a Electronics and Microelectronics, Instrumentation.
|
| 650 |
2 |
4 |
|a Control, Robotics, Mechatronics.
|
| 650 |
2 |
4 |
|a Systems Theory, Control.
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| 650 |
2 |
4 |
|a Automotive Engineering.
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| 700 |
1 |
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|a Edwards, Christopher.
|e editor.
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| 700 |
1 |
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|a Lombaerts, Thomas.
|e editor.
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| 700 |
1 |
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|a Smaili, Hafid.
|e editor.
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| 710 |
2 |
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|a SpringerLink (Online service)
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| 773 |
0 |
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|t Springer eBooks
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