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Small Size TDF37IMU0 Fiber Optic Inertial Unit Low Power Consumption

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Small Size TDF37IMU0 Fiber Optic Inertial Unit Low Power Consumption

Brand Name : NAVI OPTICS

Model Number : TDF37IMU0

Place of Origin : China

MOQ : one set

Payment Terms : T/T,L/C

Packaging Details : carton box

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Small Size TDF37IMU0 Fiber Optic Inertial Unit Low Power Consumption


Overview

Fiber optic inertial units have the advantages of small size, light weight, low power consumption, and high accuracy. They can be used to design pure strapdown systems, meet the needs of new unmanned platforms, water/torpedo weapons, as well as land, airborne, and missile weapon platforms for small size and high-precision inertial unit equipment, and have dynamic measurement functions for carrier angular and linear motion information.


Performance

Project

Content

Index

Remark

Performance indicators of gyroscope

Zero bias indicator

 

Zero bias stability (10s)

0.2°/h

 

Variable temperature zero bias stability (100s)

0.5°/h

 

Scale Factor

Scale factor nonlinearity

≤20ppm

 

Other indicators

random walk coefficient

0.02°/√h

 

input range

400°/s

 

Performance indicators of accelerometer

Deviation index

Zero bias repeatability

0.3mg

 

Zero bias indicator

Zero bias temperature sensitivity

50μg/℃

 

Scale Factor

 

Scale factor repeatability

300ppm

 

Scale factor temperature sensitivity

20ppm/℃

 

Range indicator

input range

±20g

 

Whole machine characteristics

Environmental performance indicators

 

operation temperature

-40℃~65℃

 

storage temperature

-40℃~60℃

 

General requirements

power supply

18~36V(DC)

 

Stable power consumption

≤8W

Startup power consumption ≤ 15W


Communication protocols

a. RS422 serial port 1IMU raw data output. Output three channels of angle increment information, three channels of speed increment information, IO count information, temperature information, with a data frequency of 200Hz (raw observation values without interpolation are compensated for errors). The data protocol is shown in Appendix A, and the output data is not lost;

b. RS422 serial port 2IMU synchronous data output. Output the time synchronization signal for sampling time 1 (valid rising edge, rising edge time represents the sampling time of the inertial sensor), RS422 differential signal, pulse width of 10 ± 2 μ s, sampling signal interval of 5ms ± 20 μ s, rising edge and falling edge level establishment time not exceeding 100ns, sending serial port 1 data after 50 μ s of rising edge emission.

c. RS422 serial port 3 gyroscope raw data output. Transmission rate: 460.8kbps ± 2kbps; Verification method: even verification; Output format: RS422; Output information: The gyroscope receives an external 2kHz square wave through the 422 interface, synchronized at the falling edge of a positive pulse (or the gyroscope sends data in broadcast form with a 2k update frequency); Scale factor: see test report.


Output Data Protocol

The raw data output frequency of IMU is 200Hz, and the protocol is as follows:

a. Baud rate: 460800bps;

b. Output format: RS422, 1-bit start bit, 1-bit stop bit, 8-bit data bit, no checksum;

c. Data frequency: 200Hz;

d. Communication Protocol: The communication protocol is detailed in the table below;

e. All undefined bits are filled with 0 by default. When transmitting multiple bytes, the low byte comes first and the high byte comes last.


Byte Number

Meaning

Data Type

Length

Description

1-4

packet header

unsigned int

4 bytes

0x55,0x55,0x55,0x55

5-8

Packet Count

unsigned int

4 bytes

IMU internal count value

9-12

X gyroscope data

Single precision floating point

4 bytes

linear measure

12-16

Y gyroscope data

Single precision floating point

4 bytes

linear measure

16-20

Z-gyroscope data

Single precision floating point

4 bytes

linear measure

21-24

Add table data to X

Single precision floating point

4 bytes

M/S

25-28

Y adds table data

Single precision floating point

4 bytes

M/S

29-32

Z adds table data

Single precision floating point

4 bytes

M/S

33-34

X adds temperature to the meter

unsigned int

2 bytes

linear measure

35

IO1 pulse counting

unsigned int

1 byte

-

36

IO2 pulse counting

unsigned int

1 byte

-

37

Sign position

unsigned int

1 byte

-

38

checksum

unsigned int

1 byte

Sum of 1-37 bytes

Note:

X. The Y-axis and Z-axis gyroscope data are angle increments, measured in degrees.

X. The data on the Y and Z axes is the speed increment, measured in meters per second.

Temperature unit: degrees, positive=(D33+D34 * 256) * 0.01, negative=(D33+D34 * 256-65536) * 0.01.

The definition of the flag is shown in Appendix 1 (b).


Electrical interfaces

The device connector model is J63A-242-015-261-TH, used for power supply and communication, and the mating plug is J63A-12-015-161-JC.


Pin

Connectivity

Signal Name

Signal Characteristics

1,2

External power supply

 

PCS power supply

24V

3,4

PCS Power Supply

Power Ground

5

200Hz signal output

 

IMU_TX1+

IMU data output positive

6

IMU_TX1-

IMU data output negative

9

Synchronization signal

IMU_SYN+

IMU synchronization signal positive

10

IMU_SYN-

IMU synchronization signal negative


Dimensions

Small Size TDF37IMU0 Fiber Optic Inertial Unit Low Power Consumption

Weight: ≤ 0.5kg


Product Tags:

small fiber optic inertial unit

      

low power IMU sensor

      

compact inertial measurement unit

      
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