Robust Mode Transition for Spacecraft Attitude Control

E Burgin, CJ Winkler, F Biertümpfel, H Pfifer… - AIAA SCITECH 2025 …, 2025 - arc.aiaa.org
This paper proposes the design of a single linear parameter-varying (LPV) controller for the
combined control and smooth transition between two modes in a spacecraft mission. Current …