Electrodynamic attitude stabilization of a satellite in the Konig frame
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Publication:330806
DOI10.1007/S11071-015-2256-1zbMath1348.70073OpenAlexW901795287MaRDI QIDQ330806
Publication date: 26 October 2016
Published in: Nonlinear Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s11071-015-2256-1
Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05) Asymptotic stability in control theory (93D20) Control of mechanical systems (70Q05) Orbital mechanics (70M20)
Related Items (5)
A control method for angular stabilization of an electrodynamic tether system ⋮ Partial stability analysis of nonlinear nonstationary systems via averaging ⋮ Attitude stabilization of a rigid body in conditions of decreasing dissipation ⋮ Averaging method in the problem of the Lorentz stabilization of the indirect equilibrium position of a satellite in the orbital coordinate system ⋮ Attitude stabilization of a rigid body under the action of a vanishing control torque
Cites Work
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- Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness
- Monoaxial electrodynamic stabilization of Earth satellite in the orbital coordinate system
- Optimizing the electrodynamical stabilization method for a man-made Earth satellite
- Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits
- Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics
- Parametric control in the problem of spacecraft stabilization in the geomagnetic field
- Problems of stabilization of nonstationary systems with incomplete feedback
- Control of chaotic motion in a spinning spacecraft with a circumferential nutational damper
- The vectorial parameterization of rotation
- On the control of programmed motion of a rigid body containing moving masses
- Robust fault-tolerant control for flexible spacecraft against partial actuator failures
- Robust finite-time control allocation in spacecraft attitude stabilization under actuator misalignment
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