Attitude analysis and robust adaptive backstepping sliding mode control of spacecrafts orbiting irregular asteroids

DOI10.1155/2014/367163zbMath1407.70031OpenAlexW1988482127WikidataQ59064664 ScholiaQ59064664MaRDI QIDQ1718201

Yuanchun Li, Chunhui Liang

Publication date: 8 February 2019

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2014/367163

Mathematics Subject Classification ID

Variable structure systems (93B12) Orbital mechanics (70M20)

Related Items (3)

Neural network control for the probe landing based on proportional integral observer ⋮ Adaptive fuzzy sliding mode control for the probe soft landing on the asteroids with weak gravitational field ⋮ Fractional Order Back Stepping Sliding Mode Control for Blood Glucose Regulation in Type I Diabetes Patients

Cites Work

• Attitude dynamics and control of satellites orbiting rotating asteroids
• Comment on a formula for the gravitational harmonic coefficients of a triaxial ellipsoid
• Sliding mode control with bounded \(\mathcal L_2\) gain performance of Markovian jump singular time-delay systems
• Adaptive backstepping sliding mode control for feedforward uncertain systems
• Dissipativity-Based Sliding Mode Control of Switched Stochastic Systems

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