docs: Codespell check on English sources + swd fixes (#26657)

This commit is contained in:
Hamish Willee
2026-03-05 12:50:59 +11:00
committed by GitHub
parent 5528ebec64
commit b37733459d
96 changed files with 180 additions and 174 deletions
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@@ -186,9 +186,9 @@ Some of GNSS terms that are useful for interpreting the data include:
- `DOP`: Dilution of position (dimensionless).
This is a measure of the geometric quality of satellite positions and their effect on the precision of the GPS receiver's calculations.
- `EPH`: Standard deviation of horizontal position error (metres).
This represents the the uncertainty in the GPS fix latitude and longitude.
This represents the uncertainty in the GPS fix latitude and longitude.
- `EPV`: Standard deviation of vertical position error (metres).
This represents the the uncertainty in the GPS fix altitude.
This represents the uncertainty in the GPS fix altitude.
### DOP vs EPH/EPV
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@@ -22,7 +22,7 @@ If it fails before flight, arming will be denied.
### Compass Parts
PX4 can be used with many magnetometer parts, including: Bosch BMM 150 MEMS (via I2C bus), HMC5883 / HMC5983 (I2C or SPI), IST8310 (I2C), LIS3MDL (I2C or SPI), RM3100, and more.
Other supported magnetometer parts and their busses can be inferred from the drivers listed in [Modules Reference: Magnetometer (Driver)](../modules/modules_driver_magnetometer.md).
Other supported magnetometer parts and their buses can be inferred from the drivers listed in [Modules Reference: Magnetometer (Driver)](../modules/modules_driver_magnetometer.md).
These parts are included in stand alone compass modules, combined compass/GNSS modules, and also in many flight controllers,
@@ -55,7 +55,7 @@ Note:
Internal compasses are not recommended for real use as a heading source, because the performance is almost always very poor.
This is particularly true on on small vehicles where the flight controller has to be mounted close to motor/ESC power lines and other sources of electromagnetic interference.
This is particularly true on small vehicles where the flight controller has to be mounted close to motor/ESC power lines and other sources of electromagnetic interference.
While they may be better on larger vehicles (e.g. VTOL), where it is possible to reduce electromagnetic interference by mounting the flight controller a long way from power supply lines, an external compass will almost always be better.
::: tip
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@@ -10,7 +10,7 @@ In addition to surveying/mapping, it is suitable for many other use-cases, inclu
- High-performance H7 processor
- High precision industrial grade IMU
- Support RTK and save RAW raw data (PPK) at the same time
- Support RTK and save raw data (PPK) at the same time
- Multi-satellite and multi-frequency receivers
- UAVCAN/Dronecan protocol
- Support hotshoe and shutter trigger
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@@ -77,7 +77,7 @@ The 1.25mm pitch 6P connector (from left: PIN1 to PIN6) supports UART for GNSS a
## Hardware Setup
RTK requires a base RTK module attached to the ground station, and a rover RTK module on the vehicle.
The data from the base needs to be transmitted to the drone via telemetry radio and inputed into the RTK receiver on the rover.
The data from the base needs to be transmitted to the drone via telemetry radio and inputted into the RTK receiver on the rover.
![RTK setup overview](../../assets/hardware/gps/datagnss_gem1305/setup_overview.png)
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@@ -26,7 +26,7 @@ For an equivalent GPS module with a compass try: [LOCOSYS Hawk R2](../gps_compas
- Fast TTFF at low signal level
- Free hybrid ephemeris prediction to achieve faster cold start
- Default 5Hz, up to 10 Hz update rate (SBAS support 5Hz only).
- Build-in super capacitor to reserve system data for rapid satellite acquisition
- Built-in super capacitor to reserve system data for rapid satellite acquisition
![LOCOSYS Hawk R1](../../assets/hardware/gps/locosys_hawk_a1/locosys_hawk_a1_gps.png)
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@@ -22,8 +22,8 @@ The fast time-to-first-fix, RTK convergence, superior sensitivity, low power con
- Fast TTFF at low signal level
- Free hybrid ephemeris prediction to achieve faster cold start
- Default 5Hz, up to 10 Hz update rate (SBAS support 5Hz only)
- Build-in super capacitor to reserve system data for rapid satellite acquisition
- Build-in 3 axis compass function
- Built-in super capacitor to reserve system data for rapid satellite acquisition
- Built-in 3 axis compass function
- Three LED indicator for Power, PPS and Data transmit
![LOCOSYS Hawk R2](../../assets/hardware/gps/locosys_hawk_a1/locosys_hawk_a1_gps.png)
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@@ -108,7 +108,7 @@ To enable multi-antenna attitude determination, follow the following procedure:
These can be compensated for with the heading parameters provided by the Septentrio driver in PX4.
::: info
For optimal heading results, the two antennas should be seperated by at least 30cm / 11.8 in (ideally 50cm / 19.7in or more).
For optimal heading results, the two antennas should be separated by at least 30cm / 11.8 in (ideally 50cm / 19.7in or more).
For additional configuration of the dual antenna setup, please refer to our [Knowledge Base](https://support.septentrio.com/l/858493/2022-04-19/xgrqd) or the [hardware manual](https://web.septentrio.com/l/858493/2022-04-19/xgrql).
:::