Linear Parameter-Varying Polytopic Modeling and Control Design for Guided Projectiles

Journal Article (2024)
Authors

Gian Marco Vinco (Université Grenoble Alpes, French-German Research Institute)

Olivier Sename (Université Grenoble Alpes)

Guillaume Strub (French-German Research Institute)

Spilios Theodoulis (TU Delft - Control & Simulation)

Research Group
Control & Simulation
To reference this document use:
https://doi.org/10.2514/1.G007726
More Info
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Publication Year
2024
Language
English
Research Group
Control & Simulation
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public. @en
Issue number
3
Volume number
47
Pages (from-to)
433-447
DOI:
https://doi.org/10.2514/1.G007726
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Abstract

In this paper, a linear parameter varying (LPV) modeling and control design approach is applied to a new class of guided projectiles, aiming to exploit the advantages of the LPV framework in terms of guaranteed stability and performance. The investigated concept consists of a planar symmetric 155 mm fin-stabilized projectile equipped with a reduced amount of control actuators and characterized by a predominantly unstable behavior across the analyzed flight envelope. A dedicated modeling procedure allows reformulating the nonlinear projectile dynamics as a LPV polytopic system, employed for the controller design. The procedure intends to reduce the computational complexity and the conservativeness affecting the overall controller synthesis. A trajectory-tracking simulation scenario is performed in a realistic simulator environment to assess the performance of the resulting LPV polytopic autopilot across the entire flight envelope.

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