Robust linear quadratic regulator via sliding mode guidance for spacecraft orbiting a tumbling asteroid

DOI10.1155/2015/947843zbMath1394.93295OpenAlexW2120654194WikidataQ59120002 ScholiaQ59120002MaRDI QIDQ1667025

Peng Zhang

Publication date: 27 August 2018

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

Full work available at URL: https://doi.org/10.1155/2015/947843

Mathematics Subject Classification ID

Adaptive or robust stabilization (93D21) Variable structure systems (93B12) Orbital mechanics (70M20)

Cites Work

• Exterior gravitation of a polyhedron derived and compared with harmonic and mascon gravitation representations of asteroid 4769 Castalia
• Robust sliding mode guidance and control for soft landing on small bodies
• Ellipsoidal harmonic expansions of the gravitational potential: theory and application

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