Difference between revisions of "GeoLink Introduction"
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== GNSS signal == | == GNSS signal == | ||
| − | In order to operate correctly, it is crucial to provide optimal operational conditions that are mainly secured by correct module mounting on R/C model. | + | In order to operate correctly, it is crucial to provide optimal operational conditions that are mainly secured by correct [[GeoLink_mounting|module mounting]] on R/C model. |
It is always beneficial to ensure the best conditions as it is directly related to positioning precision, GNSS signal stability and time to first fix (TTFF). Any mounting improvement that can be done is helpful. | It is always beneficial to ensure the best conditions as it is directly related to positioning precision, GNSS signal stability and time to first fix (TTFF). Any mounting improvement that can be done is helpful. | ||
| Line 18: | Line 18: | ||
Whenever powering the module it starts by searching for all nearby satellites. This procedure takes a certain period until strong enough signal is found. Length of the period is directly associated with module mounting and possible interference. | Whenever powering the module it starts by searching for all nearby satellites. This procedure takes a certain period until strong enough signal is found. Length of the period is directly associated with module mounting and possible interference. | ||
| − | If conditions are good the TTFF takes usually around 30 seconds. But thanks to advanced features implemented in GeoLink the period can be greatly reduced down to 6 seconds. Thus the module can be fully operable immediately after initialization of the Spirit unit. This is described in the Features section. | + | If conditions are good the TTFF takes usually around 30 seconds. But thanks to advanced features implemented in GeoLink the period can be greatly reduced down to 6 seconds. Thus the module can be fully operable immediately after initialization of the Spirit unit. This is described in the [[GeoLink_Features|Features section]]. |
| + | |||
| + | == Safety == | ||
| + | |||
| + | Although Spirit unit with GeoLink modules can fly with no additional steering inputs, it is always required that pilot has full control over R/C models that are operated in this way. Pilot must always watch the model while holding radio transmitter and to not allow flying anywhere where a damage could occur. All functions that the module provide can be turned off at any time and with no delay so that pilot can steer the model normally. Improper operating conditions can lead to a failure of the system. | ||
| + | <br/> | ||
| + | {{Quote|'''The user takes full responsibility for any damage or injury caused while flying an R/C model equipped with one of our devices. The manufacturer can neither guarantee nor control the conditions in which the unit is being used.'''}} | ||
Revision as of 15:35, 26 May 2018
GeoLink module is aiding peripheral for Spirit System units. It is utilizing Global Navigation Satellite System (GNSS) to acquire absolute position on Earth. To further improve precision it is embedded with Pressure, Temperature, Humidity sensors and also Gyroscope, Accelerometer and Compass sensors. All the signals are processed in a dedicated 32bit processor. This makes it extraordinary solution for R/C models.
A satellite navigation system with global coverage consists from:
- GPS
- GLONASS
- BeiDou
- Galileo
The module can use all these navigation systems at the same time. GNSS technology itself is able to provide precision of up to 2 meters. But thanks to all the algorithms and sensors it was possible to improve the precision by one order.
1 GNSS signal
In order to operate correctly, it is crucial to provide optimal operational conditions that are mainly secured by correct module mounting on R/C model. It is always beneficial to ensure the best conditions as it is directly related to positioning precision, GNSS signal stability and time to first fix (TTFF). Any mounting improvement that can be done is helpful.
2 Time To First Fix
Whenever powering the module it starts by searching for all nearby satellites. This procedure takes a certain period until strong enough signal is found. Length of the period is directly associated with module mounting and possible interference. If conditions are good the TTFF takes usually around 30 seconds. But thanks to advanced features implemented in GeoLink the period can be greatly reduced down to 6 seconds. Thus the module can be fully operable immediately after initialization of the Spirit unit. This is described in the Features section.
3 Safety
Although Spirit unit with GeoLink modules can fly with no additional steering inputs, it is always required that pilot has full control over R/C models that are operated in this way. Pilot must always watch the model while holding radio transmitter and to not allow flying anywhere where a damage could occur. All functions that the module provide can be turned off at any time and with no delay so that pilot can steer the model normally. Improper operating conditions can lead to a failure of the system.
The user takes full responsibility for any damage or injury caused while flying an R/C model equipped with one of our devices. The manufacturer can neither guarantee nor control the conditions in which the unit is being used.
