A sum-of-squares framework combined with LaSalle's principle verifies almost global asymptotic stability for spacecraft attitude control systems on non-contractible manifolds, applied to aerodynamic and gravity-gradient examples.
Analysis and design of po lynomial control systems using dissipation inequalities and sum of s quares
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Sum-of-Squares Stability Verification on Manifolds with Applications in Spacecraft Attitude Control
A sum-of-squares framework combined with LaSalle's principle verifies almost global asymptotic stability for spacecraft attitude control systems on non-contractible manifolds, applied to aerodynamic and gravity-gradient examples.