Sliding mode attitude control using thrusters and pulse modulation for the ASTER mission

DOI10.1007/S40314-014-0146-7zbMath1317.93069OpenAlexW2003022802MaRDI QIDQ2516808

Pedro Paglione, Bruno Victorino Sarli, André Luis da Silva

Publication date: 4 August 2015

Published in: Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s40314-014-0146-7

zbMATH Keywords

sliding modeattitudePWMasteroid missionnon-linear controlASTERPWPFM

Mathematics Subject Classification ID

Numerical mathematical programming methods (65K05) Nonlinear systems in control theory (93C10) Nonlinear ordinary differential equations and systems (34A34) Adaptive or robust stabilization (93D21) Control of mechanical systems (70Q05) Variable structure systems (93B12) Digital control/observation systems (93C62) Dynamical systems in control (37N35) Dynamical systems in classical and celestial mechanics (37N05) (n)-body problems (70F10)

Related Items (2)

Mathematical modeling of spacecraft guidance and control system in 3D space orbit transfer mission ⋮ Sliding mode attitude control using thrusters and pulse modulation for the ASTER mission

Cites Work

• Unnamed Item
• Sliding mode attitude control using thrusters and pulse modulation for the ASTER mission
• Variable structure systems with sliding modes
• Solar System Dynamics

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