Pages that link to "Item:Q927509"
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The following pages link to Parametric control in the problem of spacecraft stabilization in the geomagnetic field (Q927509):
Displaying 9 items.
- Electrodynamic attitude stabilization of a satellite in the Konig frame (Q330806) (← links)
- Monoaxial electrodynamic stabilization of Earth satellite in the orbital coordinate system (Q462045) (← links)
- Parametric excitation induced by solar pressure torque on the roll-yaw attitude motion of a gravity-gradient stabilized spacecraft (Q642415) (← links)
- Optimizing the electrodynamical stabilization method for a man-made Earth satellite (Q650035) (← links)
- A control method for angular stabilization of an electrodynamic tether system (Q827911) (← links)
- Attitude stabilization of a rigid body in conditions of decreasing dissipation (Q1742124) (← links)
- Electrodynamic stabilization of artificial Earth satellites in the König coordinate system (Q1743046) (← links)
- Averaging method in the problem of the Lorentz stabilization of the indirect equilibrium position of a satellite in the orbital coordinate system (Q2038524) (← links)
- Discussion on: `Optimal magnetic momentum control for inertially pointing spacecraft' (Q2512131) (← links)