Launcher attitude control: discrete-time robust design and gain-scheduling

Olivier Voinot; Daniel Alazard; Pierre Apkarian; Sophie Mauffrey; Benoît Clément

doi:10.1016/S0967-0661(02)00234-4

Launcher attitude control: discrete-time robust design and gain-scheduling

Olivier Voinot, Daniel Alazard, Pierre Apkarian, Sophie Mauffrey, Benoît Clément

Research output: Contribution to journal › Article › peer-review

17 Citations (Scopus)

Abstract

In this paper, a robust multi-objective design for the control of a launcher during atmospheric flight is investigated. This approach is based on the Cross Standard Form formulation which allows to incorporate the various specifications of the launcher problem in a streamlined manner. An important feature of this approach is that a non-conventional LQG/LTR approach, required to satisfy time-domain specifications, can be embedded into a more general standard problem in order to account for frequency-domain robustness constraints. The specific form of this standard problem is also very interesting for gain scheduling.

Original language	English
Pages (from-to)	1243-1252
Number of pages	10
Journal	Control Engineering Practice
Volume	11
Issue number	11
DOIs	https://doi.org/10.1016/S0967-0661(02)00234-4
Publication status	Published - Nov 2003
Externally published	Yes

Keywords

Cross standard form
Gain scheduling
Launcher
Multi-objective design
Robustness

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AU - Mauffrey, Sophie

AU - Clément, Benoît

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KW - Gain scheduling

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KW - Multi-objective design

KW - Robustness

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Launcher attitude control: discrete-time robust design and gain-scheduling

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Keywords

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