Aerospace launch vehicle control: A gain scheduling approach

Benoît Clement; Gilles Duc; Sophie Mauffrey

doi:10.1016/j.conengprac.2003.12.013

Aerospace launch vehicle control: A gain scheduling approach

Benoît Clement, Gilles Duc, Sophie Mauffrey

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

29 Citations (Scopus)

Abstract

This paper presents a methodology for designing an aerospace launch vehicle autopilot. Linear controllers are first designed using a multi-objective method based on the Youla parameterization and the optimization under constraints described by linear matrix inequalities. These controllers are then interpolated in such a way that the stability of the closed-loop plant is guaranteed. Results obtained from a nonlinear simulator against wind disturbances and parameter uncertainties are then given.

Original language	English
Pages (from-to)	333-347
Number of pages	15
Journal	Control Engineering Practice
Volume	13
Issue number	3
DOIs	https://doi.org/10.1016/j.conengprac.2003.12.013
Publication status	Published - Mar 2005
Externally published	Yes

Keywords

Aerospace launch vehicle
Discrete-time systems
Gain scheduling
Interpolation
Linear matrix inequalities
Multi-objective control

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10.1016/j.conengprac.2003.12.013Licence: In Copyright

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Aerospace launch vehicle control: A gain scheduling approach

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Keywords

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