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TY-MIMU05A

The Chongqing Tianjian Inertial Technology Co., Ltd. TY-MIMU05A is a compact MEMS inertial measurement unit for UAV applications. Combining gyroscope and accelerometer sensing with ARM processing, it supports angular velocity, acceleration and attitude outputs, plus self-test and inertial navigation functions.

Tianjian InertialDrone flight controller
Application
Suitable for UAV applications.
Weight
≤65g
Dimensions
40 mm × 40 mm × 16 mm

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Product overview

The TY-MIMU05A measures inertial information using a MEMS gyroscope and MEMS accelerometer, supporting angular velocity, acceleration and attitude-angle outputs for UAV applications. Its construction brings together these sensors with an ARM processor, power circuitry, interfaces and a structural body. The unit uses a miniaturized, low-power design with high reliability and strong environmental adaptability. Self-test capability accompanies an inertial navigation function that provides position, velocity and attitude information.

The gyroscope has a measurement range of ±500°/s and bias stability of ≤5°/h with 10 s smoothing at 1σ. The accelerometer provides a ±30g measurement range and bias stability of ≤0.5mg under the same 10 s smoothing and 1σ conditions. Measuring 40mm × 40mm × 16mm and weighing ≤65g, the TY-MIMU05A combines its inertial sensing, processing and interface components in a compact structural body.

Flight control & navigation

Specifications

TY-MIMU05A specifications
SpecificationValue & conditions
Product typeTY-MIMU05A inertial measurement unit
Gyroscope measurement range±500°/s
Gyroscope bias stability≤5°/h10 s smoothing, 1σ.
Accelerometer measurement range±30g
Accelerometer bias stability≤0.5mg10 s smoothing, 1σ.
Weight≤65g
Dimensions40mm × 40mm × 16mm
Measurement outputsSupports angular velocity, acceleration and attitude-angle outputs.
ConstructionMEMS gyroscope, MEMS accelerometer, ARM processor, power circuitry, interfaces and structural body.
DesignMiniaturized, low-power design with high reliability and strong environmental adaptability.
ApplicationSuitable for UAV applications.
Self-testSelf-test capability.
Inertial navigationInertial navigation capability with position, velocity and attitude outputs.

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