Pages that link to "Item:Q733932"
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The following pages link to Stabilization of a wheels carrying communication satellite without angle and angular velocity sensors (Q733932):
Displaying 9 items.
- Unloading angular momentum for inertial actuators of a spacecraft in the pitch channel (Q357805) (← links)
- On the stabilization of a communication satellite without measuring its angular velocity (Q395487) (← links)
- On an adaptive control system for angular motion of a communication satellite (Q734243) (← 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)
- Controlling a satellite using single-gimbal control moment gyroscope during their spinning and braking (Q786153) (← links)
- Application of generalized Butterworth polynomials for stabilization of the equilibrium position of a space station (Q786175) (← links)
- Accuracy testing of magnetic stabilization of small satellites (Q1596179) (← links)
- On the rapid orbital attitude control of manned and cargo spacecraft \textit{Soyuz MS} and \textit{Progress MS} (Q1745893) (← links)
- Studying the possibility of ensuring the stabilization accuracy characteristics of an advanced spacecraft for remote sensing of the Earth (Q1994814) (← links)
