Robust Autopilot Design by Structured H∞ Loop Shaping

An Agile Aerospace Vehicle Application

Master thesis (2024)

Authors

C. Loukisas Aerospace Engineering

Contributors

S.T. Theodoulis (supervisor 1)
Max Mulder (supervisor 2)
E. Mooij Astrodynamics & Space Missions - Aerospace Engineering (supervisor 2)
Faculty
Aerospace Engineering
Copyright: © 2024 Chari Loukisas
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Published Date

31-01-2024

Language

English

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Faculty

Aerospace Engineering

Abstract

This study demonstrates an effective systematic control design procedure by applying H∞ Loop-Shaping with a structured controller on an agile aerospace vehicle with a focus on automation. The gain-scheduled implementation is additionally described and tested with non-linear simulations, including a realistic moving point-hit scenario with guidance. The imposed robustness and performance requirements are met for most linear design points and for the non-linear simulations. The resulting autopilot design procedure is deemed effective in both the design procedure and implementation. It is subject to certain recommendations for improvement and extension.