From Standard to Structured Robust Control Design: Application to Aircraft Automatic Glide-slope Approach

Pedro Simplicio; Diego Navarro-Tapia; Andrea Iannelli; Andres Marcos

From Standard to Structured Robust Control Design: Application to Aircraft Automatic Glide-slope Approach

Pedro Simplicio, Diego Navarro-Tapia, Andrea Iannelli, Andres Marcos

Research output: Contribution to conference › Conference Paper › peer-review

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Abstract

The newly-developed structured H_∞ paradigm provides a powerful and versatile tool for multi-variable/multi-requirement control synthesis, with successful applications growing rapidly. However, due to its versatility, insights arising naturally from the standard (i.e., unstructured) H_∞ framework as well as other design choices are easily overlooked. Hence, this paper shows how this type of information can be exploited to have better systematic understanding and control solutions. As application scenario, the design and analysis of a robust glide-slope approach controller is addressed. This controller is part of a complete automatic landing system developed under the scope of an aircraft landing challenge proposed by ONERA and AIRBUS.

Original language	English
Number of pages	6
Publication status	Unpublished - 3 Sept 2018
Event	9th IFAC Symposium on Robust Control Design (ROCOND 2018) - Florianópolis, Brazil Duration: 3 Sept 2018 → 5 Sept 2018

Conference

Conference	9th IFAC Symposium on Robust Control Design (ROCOND 2018)
Country/Territory	Brazil
City	Florianópolis
Period	3/09/18 → 5/09/18

Keywords

Structured control design
robust control analysis
aircraft landing challenge

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title = "From Standard to Structured Robust Control Design: Application to Aircraft Automatic Glide-slope Approach",

abstract = "The newly-developed structured H∞ paradigm provides a powerful and versatile tool for multi-variable/multi-requirement control synthesis, with successful applications growing rapidly. However, due to its versatility, insights arising naturally from the standard (i.e., unstructured) H∞ framework as well as other design choices are easily overlooked. Hence, this paper shows how this type of information can be exploited to have better systematic understanding and control solutions. As application scenario, the design and analysis of a robust glide-slope approach controller is addressed. This controller is part of a complete automatic landing system developed under the scope of an aircraft landing challenge proposed by ONERA and AIRBUS.",

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T1 - From Standard to Structured Robust Control Design

T2 - 9th IFAC Symposium on Robust Control Design (ROCOND 2018)

AU - Simplicio, Pedro

AU - Navarro-Tapia, Diego

AU - Iannelli, Andrea

AU - Marcos, Andres

PY - 2018/9/3

Y1 - 2018/9/3

N2 - The newly-developed structured H∞ paradigm provides a powerful and versatile tool for multi-variable/multi-requirement control synthesis, with successful applications growing rapidly. However, due to its versatility, insights arising naturally from the standard (i.e., unstructured) H∞ framework as well as other design choices are easily overlooked. Hence, this paper shows how this type of information can be exploited to have better systematic understanding and control solutions. As application scenario, the design and analysis of a robust glide-slope approach controller is addressed. This controller is part of a complete automatic landing system developed under the scope of an aircraft landing challenge proposed by ONERA and AIRBUS.

AB - The newly-developed structured H∞ paradigm provides a powerful and versatile tool for multi-variable/multi-requirement control synthesis, with successful applications growing rapidly. However, due to its versatility, insights arising naturally from the standard (i.e., unstructured) H∞ framework as well as other design choices are easily overlooked. Hence, this paper shows how this type of information can be exploited to have better systematic understanding and control solutions. As application scenario, the design and analysis of a robust glide-slope approach controller is addressed. This controller is part of a complete automatic landing system developed under the scope of an aircraft landing challenge proposed by ONERA and AIRBUS.

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KW - robust control analysis

KW - aircraft landing challenge

M3 - Conference Paper

Y2 - 3 September 2018 through 5 September 2018

ER -

From Standard to Structured Robust Control Design: Application to Aircraft Automatic Glide-slope Approach

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Conference

Keywords

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