Pages that link to "Item:Q295600"
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The following pages link to Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators (Q295600):
Displaying 10 items.
- Output control of the spectrum of a descriptor dynamical system (Q334399) (← links)
- Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel (Q357805) (← links)
- Implementation of the orbital orientation mode of an artificial satellite of the Earth without accumulation of the angular momentum of the gyro system (Q786109) (← links)
- Stabilization of the solar orientation mode of an artificial satellite of the Earth without accumulation of the angular momentum of the gyro system (Q786176) (← links)
- LMI-based criteria of controllability and observability for a descriptor MIMO system (Q1647447) (← links)
- On the solution of the attitude control problem for a space station by means of inertial actuators with working fluid. (Q1874997) (← links)
- Selection of geometric parameters of an reaction wheel system positioning when controlling the angular motion of a spacecraft (Q2134335) (← links)
- A dual-wheel multi-mode spacecraft actuator for near-minimum-time large angle slew maneuvers (Q2853531) (← links)
- Attitude Motion of Asymmetric Dual-Spin Spacecraft (Q3327802) (← links)
- Attitude Control of a Spacecraft with Two Reaction Wheels (Q5699632) (← links)
