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High Accuracy TDF72IMU0 Fiber Optic Inertial Unit Full Dynamic Motion Measurement

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High Accuracy TDF72IMU0 Fiber Optic Inertial Unit Full Dynamic Motion Measurement

Brand Name : NAVI OPTICS

Model Number : TDF72IMU0

Place of Origin : China

Payment Terms : L/C,T/T

Packaging Details : carton box

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High Accuracy TDF72IMU0 Fiber Optic Inertial Unit Full Dynamic Motion Measurement


Overview

This type of fiber optic inertial unit contains eight points of vibration reduction, which can meet the application scenarios of large impact and large vibration. It has the advantages of small size, light weight, low power consumption, and high accuracy. It has the dynamic measurement function of carrier angular and linear motion information for the use of small volume and high-precision inertial unit equipment in water/torpedo weapons, as well as land, airborne, and missile weapon platforms.


Performance

Project

Contents

Index

Notes

Performance indicators of gyroscope

Zero bias indicator

Zero bias stability (100s)

0.01°/h

Zero bias stability (10s)

0.03°/h

Variable temperature zero bias stability

0.05°/h

Scale Factor

Full temperature scale factor

≤150ppm

Other indicators

Random walk coefficient

0.002°/h

Input range

400°/s

Performance indicators of accelerometer

Deviation index

Deviation monthly comprehensive error

20μg

Zero bias indicator

Zero bias temperature sensitivity

20μg/℃

Scale Factor

Scale factor monthly comprehensive error

20ppm

Scale factor temperature sensitivity

20ppm/℃

Range indicator

Input range

±20g

Whole machine characteristics

Environmental performance indicators

Operation temperature

-40℃~60℃

Storage temperature

-45℃~70℃

General requirements

Power supply

18~36V(DC)

Stable power consumption

≤15W

Startup power consumption ≤ 25W


Communication protocols

The baud rate of the debugging data output by the software is 460800, with 8 data bits and 1 stop bit, no checksum, and sent in low to high order. General debugging data includes IMU raw data, user command data, satellite navigation record data, navigation result data, etc. The specific agreement is as follows.


SN

Message content

Type

Note

1~2

frame header

char

0x5A,0x54

3

frame length

char

0x1E

4

Frame ID

char

0x04

5~8

Frame Number

int

200Hz accumulation

9~11

X accelerometer output

char×3

Note 1

12~14

Y accelerometer output

char×3

15~17

Z accelerometer output

char×3

18~20

X gyroscope output

char×3

Note 2

21~23

Y gyroscope output

char×3

24~26

Z-gyroscope output

char×3

27

reserve

char

28~31

reserve

int

32~33

reserve

short

34

checksum

Total of 4-33 bytes


Note 1: Calculation method for speed increment

(1)The 5ms velocity increment value output by the accelerometer at time tk is yk (unit: m/s);

(2)Define the initial value of speed increment accumulation SumVelInt=0;

(3)Define Yk=int [yk × 1e5+δ Yk-1], where int [·] represents rounding operation, and δ Yk-1 represents the remainder after rounding the velocity increment in the previous step;

(4)The remainder after rounding Yk: δ Yk=yk × 1e5+δ Yk-1-Yk;

(5)SumVelInt = SumVelInt + Yk;

(6)Integer range limitation for SumVelInt:

If SumVelInt ≥ 1e7, SumVelInt=SumVelInt -1e7;

If SumVelInt<0, SumVelInt=SumVelInt+1e7;

After integer processing, limit the range of SumVelInt values to [0,1e7);

(7)Send the last 3 bytes of SumVelInt after integer processing.

Note 2: Calculation method for angle increment

(1)The 5ms angular increment value of the gyroscope output at time tk is xk (unit: rad);

(2)Define the initial value SumAngInt for angle increment accumulation as 0;

(3)Define Xk=int [xk × 1e7+δ Xk-1], where int [·] represents the rounding operation, and δ Xk-1 represents the remainder after rounding the previous angular increment;

(4)The remainder after rounding Xk: δ Xk=xk × 1e7+δ Xk-1-Xk;

(5)SumAngInt = SumAngInt + Xk;

(6)The integer range limitation of SumAngInt:

If SumAngInt ≥ 1e7, SumAngInt=SumAngInt -1e7;

If SumAngInt<0, SumAngInt=SumAngInt+1e7;

After integer processing, limit the range of SumAngInt values to [0,1e7);

(7)Send the last 3 bytes of SumAngInt after integer processing.


Electrical interfaces

The external electrical interfaces of the inertial group equipment include power interface RS422 communication interface and 100Mbps Ethernet interface. The socket model for the external electrical interface is J30JM-37ZKP, and the matching plug model is J30J-37TJL.


Pin

Connectivity

Signal name

Signal characteristics

1,2

External power supply

PCS power supply positive

24V

3,4

PCS power supply ground

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

High Accuracy TDF72IMU0 Fiber Optic Inertial Unit Full Dynamic Motion Measurement

Dimensions: 160mm × 160mm × 115mm (± 1mm, excluding connectors)

Weight: ≤ 3kg


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