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TJ-MINS100S

The Chongqing Tianjian Inertial Technology Co., Ltd. TJ-MINS100S is a MEMS integrated inertial navigation system combining a surveying-grade satellite receiver with three-axis inertial sensors. Built for applications including vehicle navigation, surveying and stabilization, it incorporates GPS/BeiDou reception, post-processing support, 12-32V input and IP65 protection.

Tianjian InertialDrone flight controller
Applications
Assisted driving, autonomous driving, vehicle positioning and heading, AGVs, power-line inspection, platform stabilization, surveying and measurement, and precision agriculture
Input voltage
12-32 V
Weight
≤0.4g
Dimensions
110 mm×81 mm×50 mm
Ingress protection
IP65

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Product overview

The Chongqing Tianjian Inertial Technology Co., Ltd. TJ-MINS100S combines inertial sensing and satellite navigation in an integrated INS/GNSS design. Its internal hardware comprises a high-precision surveying-grade satellite receiver board, a three-axis MEMS gyroscope and a three-axis MEMS accelerometer, with a built-in GPS/BeiDou dual-mode receiver. The compact system measures 110mm×81mm×50mm, supports post-processing calculations and has interfaces designed for vehicle-mounted and autonomous-driving applications. Uses include assisted driving, AGVs, vehicle positioning and heading, surveying, precision agriculture, power-line inspection and platform stabilization.

Speed accuracy is 0.03m/s, while heading accuracy is 0.2° with a single antenna or 0.1° with dual antennas. Pitch and roll accuracy are each 0.1° with good GNSS/BeiDou signals. The system maintains position, velocity and attitude accuracy for extended periods in environments affected by satellite signal obstruction or multipath. A 12-32V input range, IP65 protection and resistance to electromagnetic interference complement its integrated construction. Further applications include vehicle navigation, street-view capture, power inspection and stabilization control.

Flight control & navigation

Specifications

TJ-MINS100S specifications
SpecificationValue & conditions
Product typeTJ-MINS100S MEMS integrated inertial navigation system
Internal componentsHigh-precision surveying-grade satellite receiver board, three-axis MEMS gyroscope and three-axis MEMS accelerometer
Speed accuracy0.03m/s
Heading accuracy0.2°Single antenna.
Heading accuracy0.1°Dual antennas.
Pitch accuracy0.1°Good GNSS/BeiDou signals.
Roll accuracy0.1°Good GNSS/BeiDou signals.
Weight≤0.4g
Dimensions110mm×81mm×50mm
Post-processingSupports post-processing calculations
Interface designInterfaces designed for vehicle-mounted and autonomous-driving applications
Satellite receiverBuilt-in GPS/BeiDou dual-mode receiver
Navigation architectureIntegrated INS/GNSS design
Input voltage12-32V
Ingress protectionIP65
Electromagnetic interference resistanceResistant to electromagnetic interference
Navigation continuityMaintains position, velocity and attitude accuracy for extended periodsSatellite signal obstruction or multipath environments.
ApplicationsAssisted driving, autonomous driving, vehicle positioning and heading, AGVs, power-line inspection, platform stabilization, surveying and measurement, and precision agriculture
Additional applicationsVehicle navigation, power inspection, street-view capture and stabilization control

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