Robust-Control-Based Design and Comparison of an Adaptive Controller for the VEGA Launcher-Reference-Cited by-同舟云学术

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Robust-Control-Based Design and Comparison of an Adaptive Controller for the VEGA Launcher

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
language:
Short-container-title:

Author:

Navarro-Tapia Diego¹,Marcos Andres¹,Bennani Samir²,Roux Christophe³

Affiliation:

1. University of Bristol

2. ESA

3. Avio S.p.A.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0649

Reference17 articles.

1. Linear Parameter Varying Control Synthesis for the atmospheric phase VEGA launcher

2. Structured Singular-Value Analysis of the Vega Launcher in Atmospheric Flight

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design of a robust controller for the VEGA TVC using the L1-Adaptive Control;INCAS BULLETIN;2023-12-02

2. Satellite micro-launcher control: An integrated adaptive-robust and nonlinear approach;Control Engineering Practice;2022-05

3. The VEGA launcher atmospheric control problem: A case for linear parameter‐varying synthesis;Journal of the Franklin Institute;2022-01

4. Envelope Extension via Adaptive Augmented Thrust Vector Control System;Journal of Guidance, Control, and Dynamics;2021-05

5. Advanced H-infinity Synthesis for Launch Vehicle Attitude Control in Atmospheric Flight;AIAA Scitech 2021 Forum;2021-01-04

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