ChinaDroneRequest a quote →

Tianjian TY-MIMU10A

The Tianjian TY-MIMU10A from Chongqing Tianjian Inertial Technology Co., Ltd. is a compact MEMS inertial measurement unit for UAV applications. It combines gyroscope and accelerometer sensing with ARM processing, supporting angular velocity, acceleration and attitude angle outputs, plus self-test and inertial navigation functions.

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

Get a free quote

Product overview

The Tianjian TY-MIMU10A measures inertial information using a MEMS gyroscope and MEMS accelerometer. Its construction combines these sensors with an ARM processor, power circuitry, interfaces and a structural body. Designed for UAV applications, the unit supports angular velocity, acceleration and attitude angle outputs. Self-test functionality and inertial navigation capabilities extend its functions to position, velocity and attitude output.

The miniaturized, low-power unit measures 40mm × 40mm × 16mm and weighs ≤65g. Its gyroscope range is ±500°/s, with bias stability of ≤10°/h under 10 s smoothing at 1σ. The accelerometer provides a ±40g range and bias stability of ≤1.5mg under the same smoothing and statistical conditions. The design combines high reliability with strong environmental adaptability.

Flight control & navigation

Specifications

Tianjian TY-MIMU10A specifications
SpecificationValue & conditions
Product typeTianjian TY-MIMU10A inertial measurement unit
Gyroscope range±500°/s
Gyroscope bias stability≤10°/h10 s smoothing, 1σ.
Accelerometer range±40g
Accelerometer bias stability≤1.5mg10 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.
Design characteristicsMiniaturized, low-power design with high reliability and strong environmental adaptability.
ApplicationsSuitable for UAV applications.
Self-testSelf-test functionality.
Inertial navigationInertial navigation functionality with position, velocity and attitude outputs.

Related guides