QINGDAO NAVI OPTICS TECHNOLOGY CO.,LTD
                                                                                                           
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High Accuracy TDF72IMU0 Fiber Optic Inertial Unit for Full Dynamic Motion Measurement with Small Size

Price Negotiable
Price: Negotiable
MOQ: Negotiable
Delivery Time: Negotiable
Brand: NAVI OPTICS
Product Description
High Accuracy TDF72IMU0 Fiber Optic Inertial Unit
Full Dynamic Motion Measurement for demanding applications requiring precision and reliability under extreme conditions.
Product Overview
This advanced fiber optic inertial unit features eight-point vibration reduction technology, making it ideal for high-impact and high-vibration environments. The unit combines compact dimensions, lightweight construction, low power consumption, and exceptional accuracy for comprehensive dynamic measurement of carrier angular and linear motion information.
Designed for small-volume, high-precision applications across multiple platforms including water/torpedo weapons, land vehicles, airborne systems, and missile weapon platforms.
Performance Specifications
Gyroscope Performance Indicators
Parameter Specification Value Notes
Zero Bias Stability (100s) Zero bias stability 0.01°/h
Zero Bias Stability (10s) Zero bias stability 0.03°/h
Variable Temperature Zero Bias Zero bias stability 0.05°/h
Scale Factor Full temperature scale factor ≤150ppm
Random Walk Coefficient Other indicators 0.002°/h
Input Range Input range 400°/s
Accelerometer Performance Indicators
Parameter Specification Value Notes
Deviation Monthly Comprehensive Error Deviation index 20μg
Zero Bias Temperature Sensitivity Zero bias indicator 20μg/℃
Scale Factor Monthly Comprehensive Error Scale Factor 20ppm
Scale Factor Temperature Sensitivity Scale Factor 20ppm/℃
Input Range Range indicator ±20g
Unit Characteristics
Category Parameter Specification Notes
Environmental Performance Operation temperature -40℃~60℃
Environmental Performance Storage temperature -45℃~70℃
General Requirements Power supply 18~36V(DC)
General Requirements Stable power consumption ≤15W Startup power consumption ≤ 25W
Communication Protocols
The debugging data output operates at a baud rate of 460800, with 8 data bits, 1 stop bit, no checksum, and low-to-high order transmission. General debugging data includes IMU raw data, user command data, satellite navigation record data, and navigation result data.
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: Velocity Increment Calculation
  • The 5ms velocity increment value output by the accelerometer at time tk is yk (unit: m/s)
  • Define the initial value of speed increment accumulation SumVelInt=0
  • 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
  • The remainder after rounding Yk: δ Yk=yk * 1e5+δ Yk-1-Yk
  • SumVelInt = SumVelInt + Yk
  • 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)
  • Send the last 3 bytes of SumVelInt after integer processing
Note 2: Angle Increment Calculation
  • The 5ms angular increment value of the gyroscope output at time tk is xk (unit: rad)
  • Define the initial value SumAngInt for angle increment accumulation as 0
  • 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
  • The remainder after rounding Xk: δ Xk=xk * 1e7+δ Xk-1-Xk
  • SumAngInt = SumAngInt + Xk
  • 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)
  • Send the last 3 bytes of SumAngInt after integer processing
Electrical Interfaces
External electrical interfaces include power interface, RS422 communication interface, and 100Mbps Ethernet interface. Socket model: J30JM-37ZKP, matching plug model: 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
Physical Dimensions
TDF72IMU0 Fiber Optic Inertial Unit dimensional diagram and specifications
Dimensions: 160mm * 160mm * 115mm (± 1mm, excluding connectors)
Weight: ≤ 3kg

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Company QINGDAO NAVI OPTICS TECHNOLOGY CO.,LTD
Location Liando U Valley 25#, No.423, Juyang Rd, Huangdao District, Qingdao, 266425,China
Contact Person Ming Ming

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