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What is LPV Guidance for Space Re-entry Vehicles about?

This document presents a guidance method for atmospheric re-entry vehicles using a coupled linear parameter varying (LPV) and flatness-based approach. The method is applied to the nonlinear model of the European Atmospheric Re-entry Demonstrator. The guidance scheme achieves robust stability and performance even with entry point dispersions. The problem is formulated and solved using linear matrix inequalities. Monte Carlo simulations demonstrate the effectiveness of the proposed approach.

Author

Eddylson Aguilar Casquino

Language

EN