TDMG-300Pro MEMS Inertial/Satellite Integrated Navigation System

share

Introduction
TDMS-300Pro MEMS Integrated navigation system is a highly reliable and cost-effective six-axis MEMS inertial/satellite integrated navigation system, which can be widely used in the navigation, control and measurement fields represented by UAVS. TDMS-300Pro integrated navigation system is mainly composed of three-axis MEMS gyroscope, three-axis MEMS accelerometer, information processing circuit, navigation software, structural components, test cable, test software, GNSS receiver (built-in).

The TDMS-300Pro MEMS series integrated navigation system integrates high-performance MEMS gyroscopes and MEMS accelerometers in a separate structure that can replace the fiber optic gyro. The gyroscopes and accelerometers selected for the system represent the leading level of MEMS inertial devices. High performance gyroscope is integrated in the system, which can realize the initial state self-seeking north without auxiliary heading measures such as double antenna receiver, so as to rapidly converge and maintain high precision in the process of dynamic integrated navigation. The zero position of all temperature parameters, scale factor, non-orthogonal error and acceleration related terms are compensated in the system, which can maintain high measurement accuracy for a long time. At the same time, adaptive attitude algorithm is integrated in the system, which can ensure the measurement accuracy of attitude for a long time.
The following outputs are provided by default: 3D angular velocity, 3D acceleration, gyro temperature, accelerometer temperature, 3D attitude, INS/GNSS position, INS/GNSS speed.

Features
● GNSS receiver built-in
● Small size, low weight, low power consumption
● -40℃ to +80℃ full temperature scale compensation
● 1KHz high speed sampling rate
● Built-in adaptive attitude algorithm
● Resistant to harsh mechanical environment
● Online software upgrade function
● Inertial /GNSS integrated navigation function

Application fields
● Medium and long endurance UAVs
● Vehicle positioning and orientation
● Radar/infrared antenna stabilization platform
● Patrol Smart Munition
● Port measurement system
● Mobile communication
● UAV/Vehicle/ship/boat attitude reference
● Attitude control
● Photoelectric pod
● Steady control and sighting equipment 

Request for Quotation Request for Information

Specification

MEMS Gyroscope

Measurement range(°/s)

400

Full Temperature bias(°/h)

2

Bias stability(°/h,10s smooth)

0.3

Bias repeatability(°/h)

0.3

Non-linearity of scale factor(ppm)

100

Bandwidth(Hz)

100

MEMS Accelerometer

Measurement range(g)

30

Full Temperature bias(mg)

2

Bias stability(μg)

100

Bias repeatability(μg)

100

Non-linearity of scale factor(ppm)

500

Bandwidth(Hz)

100

Attitude Accuracy

Pitch(°,RMS)

0.05(GNSS aided)

Roll(°,RMS)

0.05(GNSS aided)

Heading(°,RMS,GNSS aided,Dynamic condition)

0.1

Electrical/Mechanical Interface

Power supply(V)

5V~12V

Power consumption(W)

3

Start-up time(s)

2

Communication port

2 x RS-422

Updating rate(Hz)

200Hz

Size(mm×mm×mm)

56mm×56mm×33.1mm

Weight(g)

≤200

Environmental Condition

Working Temperature(℃)

-40~80

Storage Temperature(℃)

-55~85

PIN definition

PIN No.

Definition

Note

1

VSUP

Power +,5-12V

2

COM1_Rx+

RS422-1 Receive +

3

COM1_Tx+

RS422-1 Transit +

4

COM2_Rx+

RS422-2 Receive +

5

COM2_Tx+

RS422-2 Transit +

6

GND

Power Ground

7

COM1_Rx-

RS422-1 Receive -

8

COM1_Tx-

RS422-1 Transit -

9

COM2_Rx-

RS422-2 Receive -

10

COM2_Tx-

RS422-2 Transit -

REQUEST FOR
quotation

+852 51098791

Contact

Thank you for your message and we will contact you within 24 Hours of your submission to resolve your issue

Online consultation