●System-level packaged integrated navigation chip
●Integrated satellite navigation chip and 6-axis inertial sensor
● Operating temperature: -40℃~+80℃
● ±16g accelerometer and three-axis ±4000°/s gyroscope
● Output mode: TTL
Shared：
IMU parameters | unit | |||||
gyroscope | range | °/s | 250 | |||
angle random walk | °/√h | 0.5 | ||||
Zero-bias instability | °/h | 5 | ||||
Full temperature zero bias | °/s | 0.3 | ||||
Scale error | - | 4‰ | ||||
Three-axis orthogonal coupling error | - | 1.7‰（0.1°） | ||||
accelerometer | range | g | ±16 | |||
rate random walk | m/s/√h | 0.3 | ||||
Zero-bias instability | μg | 50 | ||||
Full temperature zero bias | mg | 5 | ||||
Scale error | - | 2‰ | ||||
Three-axis orthogonal coupling error | - | 0.9‰（0.05°） | ||||
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