Aerospace launch vehicle control: A gain scheduling approach

Benoît Clement; Gilles Duc; Sophie Mauffrey; Arnaud Biard

doi:10.3182/20020721-6-es-1901.01249

Aerospace launch vehicle control: A gain scheduling approach

Benoît Clement
, Gilles Duc
, Sophie Mauffrey
, Arnaud Biard

Research output: Contribution to journal › Conference article › peer-review

1 Citation (Scopus)

Abstract

This paper presents a design methodology for an aerospace launch vehicle autopilot. The non stationary characteristics during the atmospheric flight impose to use a gain scheduled approach for a Linear Time Varying System (LTV). The important result is that the chosen interpolation is forced to be linear and the stability is guaranteed.

Original language	English
Pages (from-to)	145-150
Number of pages	6
Journal	IFAC Proceedings Volumes (IFAC-PapersOnline)
Volume	35
Issue number	1
DOIs	https://doi.org/10.3182/20020721-6-es-1901.01249
Publication status	Published - 2002
Externally published	Yes
Event	15th World Congress of the International Federation of Automatic Control, 2002 - Barcelona, Spain Duration: 21 Jul 2002 → 26 Jul 2002

Keywords

Aerospace launch vehicle
Discrete-time systems
Gain scheduling
Interpolation

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10.3182/20020721-6-es-1901.01249Licence: In Copyright

Cite this

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title = "Aerospace launch vehicle control: A gain scheduling approach",

abstract = "This paper presents a design methodology for an aerospace launch vehicle autopilot. The non stationary characteristics during the atmospheric flight impose to use a gain scheduled approach for a Linear Time Varying System (LTV). The important result is that the chosen interpolation is forced to be linear and the stability is guaranteed.",

keywords = "Aerospace launch vehicle, Discrete-time systems, Gain scheduling, Interpolation",

author = "Beno{\^i}t Clement and Gilles Duc and Sophie Mauffrey and Arnaud Biard",

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T2 - 15th World Congress of the International Federation of Automatic Control, 2002

AU - Clement, Benoît

AU - Duc, Gilles

AU - Mauffrey, Sophie

AU - Biard, Arnaud

PY - 2002

Y1 - 2002

N2 - This paper presents a design methodology for an aerospace launch vehicle autopilot. The non stationary characteristics during the atmospheric flight impose to use a gain scheduled approach for a Linear Time Varying System (LTV). The important result is that the chosen interpolation is forced to be linear and the stability is guaranteed.

AB - This paper presents a design methodology for an aerospace launch vehicle autopilot. The non stationary characteristics during the atmospheric flight impose to use a gain scheduled approach for a Linear Time Varying System (LTV). The important result is that the chosen interpolation is forced to be linear and the stability is guaranteed.

KW - Aerospace launch vehicle

KW - Discrete-time systems

KW - Gain scheduling

KW - Interpolation

UR - https://www.scopus.com/pages/publications/84945581655

U2 - 10.3182/20020721-6-es-1901.01249

DO - 10.3182/20020721-6-es-1901.01249

M3 - Conference article

AN - SCOPUS:84945581655

SN - 1474-6670

VL - 35

SP - 145

EP - 150

JO - IFAC Proceedings Volumes (IFAC-PapersOnline)

JF - IFAC Proceedings Volumes (IFAC-PapersOnline)

IS - 1

Y2 - 21 July 2002 through 26 July 2002

ER -

Aerospace launch vehicle control: A gain scheduling approach

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Keywords

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