Model Reference Adaptive Control Design for the VEGA Launch Vehicle

Boglis, Ioana-Carmen; Stoica, Adrian–Mihail

doi:10.1109/ehb47216.2019.8970009

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Figure 1: Typical Bending Modes1

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2020

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“…The control system is composed of a PD regulator and a Model Reference Adaptive Algorithm and it is shown in figure 2. The algorithm and the values of the parameters used are described in [13]. As the uncertainties and errors in modeling are inevitable and the parameters may vary over time, the control systems must satisfy a certain degree of robustness and adaptability.…”

Section: Figure 1: Typical Bending Modesmentioning

confidence: 99%

Attenuation of the effects produced by the bending modes of a flexible launch vehicle using second order filters

Boglis

Stoica

2020

Technium

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This article describes the application of an adaptive control algorithm for the atmospheric phase control of a launch vehicle. A dynamic model representing the pitch motion of the launch vehicle is introduced. As the bending modes can cause instability, the first threebending modes are modelled. A case study on design of the bending filters for a flexible launch vehicle using a model reference adaptive control is conducted to demonstrate its effectiveness.

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Section: Figure 1: Typical Bending Modesmentioning

confidence: 99%