NAV40 Inertial Navigation System (INS)
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NAV40 Inertial Navigation System (INS)
The NAV40 Inertial navigation system is Integrated with a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, GPS receiver module, barometric altimeter, and other miniature sensors, with information fusion achieved through the built-in improved Extended Kalman Filter (EKF).
It is specifically optimized for drone inertial navigation systems, effectively reducing the influence of vehicle maneuver, vibration, environmental temperature, and electromagnetic interference. This ensures the provision of complete and reliable three-dimensional position, three-axis attitude, three-axis velocity, three-axis acceleration, and other information at up to 200Hz.
- Dual- redundancyย
- Support external differential GPS
- support external magnetic compass
- Support external dual antenna GPS orientation
- Optional simultaneous output of attitude information under different coordinate systems
- Navigation data update frequency up to 200Hz
- Small dimension (61x40x19mm), and lightweight (45g)
Specifications
attitude angle |
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Heading |
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GNSS |
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Gyro |
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Accelerometer |
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Magnetometer |
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Power |
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Data interface |
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environmental adaptability |
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Physical parameters |
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Product contents
Pleaseย contact usย for more information.
Documents
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1 review for NAV40 Inertial Navigation System (INS)
Clear filtersWeight | 1 kg |
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Dimensions | 7 × 5 × 2 cm |
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Ava Murphy –
Il prodotto รจ di ottima qualitร , molto felice!