Application of the H∞ control theory to space missions in engineering education | Zendy

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Application of the H∞ control theory to space missions in engineering education

Author(s) -

David Henry

Publication year - 2020

Publication title -

ifac-papersonline

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.308

H-Index - 72

eISSN - 2405-8971

pISSN - 2405-8963

DOI - 10.1016/j.ifacol.2020.12.1663

Subject(s) - aerospace , interfacing , controller (irrigation) , aerodynamics , space (punctuation) , simulation , aerospace engineering , computer science , control engineering , control (management) , aeronautics , systems engineering , engineering , artificial intelligence , agronomy , computer hardware , biology , operating system

This paper is a training paper for aerospace engineering education⁎. Its aim is to give the necessary backgrounds for the application of the mixed-sensitivity approach of the robust H∞ control theory, to space missions. As a support example, the auto-landing phase of a re-entry mission is considered. The considered re-entry vehicle is the HL-20. The paper covers all the aspects of the engineer exercise, i.e. from establishing the non-linear model of the vehicle, considering especially the aerodynamic coefficients, until the implementation of the robust H∞ controller in the simulator, with a graphical interfacing with the FlightGear flight simulator.

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