Nonlinear attitude control of flexible spacecraft under disturbance torque

DOI10.1016/0094-5765(86)90029-9zbMath0597.70029OpenAlexW2021742632MaRDI QIDQ3731084

Sahjendra N. Singh

Publication date: 1986

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(86)90029-9

zbMATH Keywords

feedback pathdisturbance torqueslewing maneuvercontrol law for large-angle single-axis rotational maneuversspacecraft- beam-tip body

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Control of mechanical systems (70Q05) Kinematics of mechanisms and robots (70B15) Control/observation systems governed by ordinary differential equations (93C15)

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Adaptive robust tracking for flexible spacecraft in presence of disturbances

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