Quaternion feedback for spacecraft large angle maneuvers

DOI10.2514/3.19988zbMath0632.93053OpenAlexW2076578526MaRDI QIDQ3770406

Peter M. Barba, Bong Wie

Publication date: 1985

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.19988

zbMATH Keywords

Lyapunov stability theoremquaternion feedbacklarge angle feedback reorientation maneuversreaction jets

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Application models in control theory (93C95) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05) Stability of solutions to ordinary differential equations (34D20) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (11)

Passivity Based Attitude Control of Rigid Bodies ⋮ Passive attitude control of flexible spacecraft from quaternion measurements ⋮ Optimal geometric motion planning for a spin-stabilized spacecraft ⋮ Null‐space‐based optimal control reallocation for spacecraft stabilization under input saturation ⋮ A singular adaptive attitude control with active disturbance rejection ⋮ A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon ⋮ Discussion on: ``Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft ⋮ Optimal control on Lie groups with applications to attitude control ⋮ Spacecraft attitude control by combination of various torquers ⋮ Spacecraft attitude control using explicit model predictive control ⋮ Mathematical Modeling of the Dynamics of a Low-Flying Spacecraft with a Ramjet Electric Propulsion Engine

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