Uniform Exponential Stability Result for the Rigid-Spacecraft Attitude Tracking Control Problem (IAA-AAS-SciTech2018-051 — AAS 18-801)
IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials ; 1. ; 2018 ; Moskau
2020
Conference paper
English
Predetermined time attitude tracking control for rigid spacecraft
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