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en:w_subsys [2017/11/16 21:15] writer created |
en:w_subsys [2019/09/16 15:37] golikov |
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Virtual [[power_subsys|consumption]] - 40mA | Virtual [[power_subsys|consumption]] - 40mA | ||
- | {{ ru:device_standart.jpg?direct&200|}} | + | {{ :ru:дус.png?direct&200| ДУС }} |
- | The sensor allows changing of spacecraft current angular velocities in three axes. Depending on the location of the sensor, one of readings, specifically, the speed of rotation around the thread, will be critical for controlling the spacecraft. Other two readings will help to estimate spacecraft center of mass oscillations relative to the local vertical. This can also be used in controlling. | + | |
+ | This sensor allows you to measure the spacecraft current angular velocities of the device in three axes. Depending on the location of the sensor, one of readings, specifically the speed of rotation around the thread, will be critical for controlling the spacecraft. The other two readings will help to estimate the oscillations of the spacecraft's center of mass relative to the local vertical axis. These readings can also be used in control of the spacecraft. | ||
The angular velocity determined by the sensor is 0.00875 degrees/second per unit [[libschsat|RAW (see the function library, hyro_request_raw)]]. | The angular velocity determined by the sensor is 0.00875 degrees/second per unit [[libschsat|RAW (see the function library, hyro_request_raw)]]. |