FSI301 FOG_GNSS Combined Inertial Navigation System

FSI301 FOG_GNSS Combined Inertial Navigation System

Domestically produced core components
High performance, small size, and low weight
High-precision FOG

Description
Main Features

 

  • Domestically produced core components
  • High performance, small size, and low weight
  • High-precision FOG
  • Vibration and shock resistance, EMI resistance
  • Operation in harsh environments
product-274-286

 

Application Fields

 

  • Radar/infrared antenna stabilized platform
  • Port surveying system
  • On-the-move communication
  • Attitude reference for UAVs/vehicles/ships/boats
  • Attitude control
  • Tunneling machine/automated coal mining

 

Product Overview

 

FSI301 is a highly reliable, cost-effective fiber-optic inertial/satellite integrated navigation system, widely applicable in fields such as high-precision vehicle-mounted platforms and long-endurance UAVs, as well as navigation, control, and measurement. The system uses closed-loop fiber optic gyroscopes (FOG) and high-precision accelerometers, combined with a professional GNSS board, to achieve real-time navigation output. The system output is compatible with mainstream post-processing software to obtain higher-precision navigation results and serve as a benchmark for research platforms.

 

Unique Technology

 

FSI301 is a highly reliable, cost-effective fiber-optic inertial/satellite integrated navigation system, widely applicable in fields such as high-precision vehicle-mounted platforms and long-endurance UAVs, as well as navigation, control, and measurement. The system uses closed-loop fiber optic gyroscopes (FOG) and high-precision accelerometers, combined with a professional GNSS board, to achieve real-time navigation output. The system output is compatible with mainstream post-processing software to obtain higher-precision navigation results and serve as a benchmark for research platforms.

 

FSI301 FOG_GNSS Combined Inertial Navigation System

 

Parameters

Fiber Optic Gyroscope

Range (°/s)

±300

Full-temperature Bias (°/h, 3σ)

≤0.03

Bias Stability (°/h, 10 s avg.)

≤0.03

Bias Instability (°/h, allan)

≤0.006

MEMS Accelerometer

Range (g)

±30

Full-temperature Bias (mg, 3σ)

≤0.5

Bias Stability (μg, 10s avg.)

≤10

Bias Instability (μg, allan, typ)

≤3

Navigation Accuracy

North-seeking Accuracy(°,1σ)

≤0.1secL

Electrical/Mechanical Interface

Power Supply (V)

18~36 (ripple ≤100mV)

Dimensions (mm×mm×mm)

177*132*99

Weight (g)

≤3500

product-356-482product-349-354

 

Introduction

 

Overview

FSI301 is a highly reliable, cost-effective fiber-optic inertial/satellite integrated navigation system, widely applicable in fields such as high-precision vehicle-mounted platforms and long-endurance UAVs, as well as navigation, control, and measurement. The system uses closed-loop fiber optic gyroscopes (FOG) and high-precision accelerometers, combined with a professional GNSS board, to achieve real-time navigation output. The system output is compatible with mainstream post-processing software to obtain higher-precision navigation results and serve as a benchmark for research platforms.

 

Features

  • Lightweight high-precision integrated navigation
  • Domestically produced core components
  • High performance, small size, and low weight
  • Uses high-precision closed-loop fiber optic gyroscopes
  • Vibration and shock resistance, and electromagnetic interference resistance
  • Sealed and reliable design ensures normal operation in harsh environments
  • Has inertial/GNSS integrated navigation capability

 

Application

  • Medium- and long-endurance UAVs
  • Vehicle-mounted positioning and orientation
  • Radar/infrared antenna stabilized platform
  • Port surveying system
  • On-the-move communication
  • Attitude reference for UAVs/vehicles/ships/boats
  • Attitude control
  • Stabilized Control and Stabilized Aiming Equipment
  • Tunneling machine/automated coal mining

 

Technical Parameters

Table1FSI301 Performance Parameters

Fiber Optic Gyroscope

Range (°/s)

±300

Full-temperature Bias (°/h, 3σ)

≤0.03

Bias Stability (°/h, 10 s avg.)

≤0.03

Bias Instability (°/h, allan)

≤0.006

Bias Repeatability (°/h)

≤0.03

Angle Random Walk (°/√h)

≤0.003

Scale Factor Nonlinearity (ppm)

≤30

Cross-coupling (rad)

≤0.001

Bandwidth (Hz)

≥200Hz

MEMS Accelerometer

Range (g)

±30

Full-temperature Bias (mg, 3σ)

≤0.5

Bias Stability (μg, 10s avg.)

≤10

Bias Instability (μg, allan, typ)

≤3

Bias Repeatability (µg)

≤10

Velocity Random Walk (m/s/√h)

≤0.01

Scale Factor Nonlinearity (ppm, ±1g)

≤100

Cross-coupling (rad)

≤0.001

Bandwidth (Hz)

≥200Hz

Navigation Accuracy

North-seeking Accuracy(°,1σ)

0.1secL

Combination Horizontal Position (m, 1σ)

≤2(single point), ≤0.02+1ppm (RTK)

Combination Heading Position (m,1σ)

≤3 (single point), ≤0.03+1ppm (RTK)

Combination Horizontal Velocity (m/s, 1σ)

≤0.05

Combination Vertical Velocity (m/s, 1σ)

≤0.1

Combination Heading (°, 1σ))

≤0.1 (dynamic)

≤0.05 (RTK, dynamic)

Combination Horizontal Attitude (°, 1σ)

≤0.01 (single-point, dynamic)

≤0.007 (RTK, dynamic)

Pure Inertial Accuracy (1σ)

1nmile/30min

Depth Measurement Accuracy

≤5 cm (marine environment)

Electrical/Mechanical Interface

Power Supply (V)

18~36 (ripple ≤100mV)

Steady-state Power (W)

≤15

Startup Time (s)

≤2

Communication Interface

RS422/RS232/USB/CAN

Update Rate (Hz)

200

Dimensions (mm×mm×mm)

177*132*99

Weight (g)

3500

Operating Environment

Operating Temperature (°C)

-40 to +60

Storage Temperature (°C)

-55 to +85

Vibration (g, Rms)

20~2000HZ, 6.06

Shock (g)

100g/1ms

Reliability

MTBF (h)

75000+

Note: The receiver can be replaced with one that has satellite-based differential capability, with positioning accuracy better than 10 cm.

 

Technical Specifications

Structure

FSI301 measures 177 × 132 × 99 mm and is mounted using M5 screws.

product-356-482

Figure1 Mechanical interface diagram of the FSI301 inertial/satellite integrated navigation system

 

The GNSS receiver antenna provides a standard model size: 154 mm × 154 mm × 64.2 mm.

product-469-539

Figure2 Mechanical interface diagram of the FSI301 system satellite antenna

 

The GNSS receiver antenna provides a strong magnetic suction base, with dimensions of 100 mm × 100 mm × 66 mm.

product-790-593

product-790-889

Figure3 Magnetic suction base diagram of the FSI301 system satellite antenna

 

Product Marking/Polarity

With the product placed horizontally, the arrow indicates the X direction, and the output coordinate system is the "front, right, down" coordinate system.

product-349-354

Figure4 coordinate System

 

Interface Definitions

The FSI301 dual satellite antenna connector is a standard SMA male connector, with the left side being the positioning antenna and the right side being the directional antenna.

FSI301 uses a J30J-51ZKW electrical connector, and the corresponding plug uses J30J-51TJL. The external interface definitions are shown in the table below:

Table2 FSI301 system interface cable pin definition

Serial No.

Pin number

Description

Meaning

External connection method

1

27

VIN

External 24V power supply

Red clip

2

28

VIN

3

1

GND

Black clip

4

2

GND

5

44

LCJ_G5V

External odometer interface (incremental odometer)

Separate wire

6

45

LCJ_GGND

7

19

LCJ_B

8

20

LCJ_A

9

32

INS_RS422_RX+

External inertial navigation RS422 main interface, can be used to configure the protocol and upload core0 navigation software.

DB9-M1-1

10

6

INS_RS422_RX-

DB9-M1-2

11

4

INS_RS422_TX+

DB9-M1-3

12

30

INS_RS422_TX-

DB9-M1-4

13

3

GGND1

DB9-M1-5

14

33

JK_COMM1_RX+

ExternalRS422isolated interface, can be used to configure protocols, uploadcore1interface software

DB9-M2-1

15

7

JK_COMM1_RX-

DB9-M2-2

16

5

JK_COMM1_TX+

DB9-M2-3

17

31

JK_COMM1_TX-

DB9-M2-4

18

8

GGND1

DB9-M2-5

19

17

BY_COMM2_RX+

External spare RS422 isolated interface

DB9-M3-1

20

42

BY_COMM2_RX-

DB9-M3-2

21

41

BY_COMM2_TX+

DB9-M3-3

22

16

BY_COMM2_TX-

DB9-M3-4

23

18

GGND1

DB9-M3-5

24

10

INS_RS232_TXD

External inertial navigation RS232 isolated interface, can be used to configure protocols and output externally 232 Protocol

DB9-M4-2

25

36

INS_RS232_RXD

DB9-M4-3

26

34

GGND1

DB9-M4-5

27

9

IMU_RS232_TXD

External IMU RS232 Isolated Interface

DB9-M5-2

28

35

IMU_RS232_RXD

DB9-M5-3

29

29

GGND1

DB9-M5-5

30

15

GPS_CFG_TXD

External GPS RS232 configuration interface, supports differential positioning.

DB9-M6-2

31

40

GPS_CFG_RXD

DB9-M6-3

32

39

GGND1

DB9-M6-5

33

11

PPS_OUT+

PPS second-pulse output isolated interface (differential & single-ended TTL)

DB9-M7-1

34

37

PPS_OUT-

DB9-M7-2

35

43

GGND1

DB9-M7-7

36

12

IO_IN

PPS pulse input isolated interface (PPS+ can be reused as single-ended LVTTL output)

DB9-M8-9

37

13

PPS_IN+

DB9-M8-3

38

38

PPS_IN-

DB9-M8-4

39

14

GGND1

DB9-M8-5

40

22

CAN1H

External CAN bus isolated interface1

DB9-M9-7

41

47

CAN1L

DB9-M9-2

42

48

GGND2

DB9-M9-3

43

21

CAN2H

External CAN bus isolated interface2

DB9-M10-7

44

46

CAN2L

DB9-M10-2

45

25

USB_DM

USB interface

Separate wire

46

51

USB_DP

47

26

USB_GND

48

23

ETH_TXD_P

100Mbps Ethernet interface

Separate wire

49

49

ETH_TXD_N

50

24

ETH_RXD_P

51

50

ETH_RXD_N

After the power supply voltage drops below the device operating threshold voltage, the power-off hold time tOFF before the next power-on shall not be less than 3 s; insufficient power-off interval may cause abnormal device startup, latch-up, or initialization failure.

 

External communication

Protocol 1: Integrated Navigation Data Protocol

FSI301 default timed broadcast output data, output frequency 200Hz, each frame of data164bytes, baud rate 460800bps,1start bits,8data bits,1stop bits, no parity. Data transmission uses a little-endian data format with the least significant byte first. A typical communication protocol is shown as follows; the communication protocol can also be customized according to user requirements.

Table3Integrated Navigation System Output Communication Protocol

Serial No.

First byte order

Number of bytes

Signal Name

Dimensional unit or content

Equivalent

Interface accuracy description

1

0

1

Header 1

Content: 55H

1

8-bit unsigned integer

2

1

1

Header 2

Content: AAH

1

8-bit unsigned integer

3

2

1

Data length

Content: A0H

1

8-bit unsigned integer

4

3

4

PCNum

Interrupt counter

1

32-bit unsigned integer

5

7

1

System status word

-

1

Self-test in progress: 0x10

self-test passed: 0x12

self-test error: 0x1F

coarse alignment: 0x33

fine alignment: 0x35

pure inertial navigation: 0x41

zero-velocity correction: 0x43

Velocity + position combined: 0x44

Velocity + position + heading combined: 0x45

Vehicle-constrained navigation: 0x46

Odometer combined navigation: 0x47

during self-calibration: 0x51, 0x53, 0x55

Self-calibration completed, criteria valid: 0x56

Self-calibration written to Flash successfully: 0x57

Self-calibration error: 0x5F.

6

8

1

Real-time status word

-

1

 

7

9

2

Reserved byte

-

1

 

8

11

4

Reserved byte

-

1

 

9

15

4

X gyroscope angular velocity

[-1000, 1000]°/s,

0.0000005

Average within the output period

10

19

4

Y gyroscope angular velocity

[-1000, 1000]°/s,

0.0000005

Average within the output period

11

23

4

Z gyroscope angular velocity

[-1000, 1000]°/s,

0.0000005

Average within the output period

12

27

4

X accelerometer acceleration

[-400m/s2,400m/s2]

0.000001

Average within the output period

13

31

4

Y accelerometer acceleration

[-400m/s2,400m/s2]

0.000001

Average within the output period

14

35

4

Z accelerometer acceleration

[-400m/s2,400m/s2]

0.000001

Average within the output period

15

39

4

Combined longitude

(-180,180]deg

0.0000001

 

16

43

4

Combined latitude

[-90,90]deg

0.0000001

 

17

47

4

Combined altitude

[-500,16384]m

0.00001

 

18

51

2

Combined North Velocity

[-1310,1310]m/s

0.005

 

19

53

2

Combined Up Velocity

[-1310,1310]m/s

0.005

 

20

55

2

Combined East Velocity

[-1310,1310]m/s

0.005

 

21

57

2

Roll Angle

[-90,90]deg

0.006

 

22

59

2

Heading Angle

[-180,180]deg

0.006

West of north is positive

23

61

2

Pitch angle

[-85,85] you

0.006

 

24

63

4

Satellite longitude

(-180,180]deg

0.0000001

 

25

67

4

Satellite latitude

[-90,90]deg

0.0000001

 

26

71

4

Satellite altitude

[-500,16384]m

0.00001

 

27

75

2

Satellite north velocity

[-1310,1310]m/s

0.005

 

28

77

2

Satellite upward velocity

[-1310,1310]m/s

0.005

 

29

79

2

Satellite east velocity

[-1310,1310]m/s

0.005

 

30

81

1

Temperature

[-127,127]

1

 

31

82

1

Positioning and orientation validity

/

1

bit0-3, receiver positioning flag:

00 no positioning,

01 single-point positioning,

02 float solution positioning,

03 fixed solution positioning; bit4-7, orientation signal:

00 no orientation,

01 single-point orientation,

02 float solution orientation,

03 fixed solution orientation.

32

83

4

Satellite time of week in seconds

     

33

87

1

Year

     

34

88

1

Month

     

35

89

1

Day

     

36

90

1

Number of positioning satellites

[0,255]

1

 

37

91

2

Satellite track angle

[-180,180]deg

0.006

 

38

93

2

Dual-antenna heading

[-180,180]deg

0.006

 

39

95

2

Reserved

     

40

97

14

Reserved

     

41

111

12

Reserved

     

42

123

4

AU

m/s²

1

Upward acceleration

43

127

4

AF

m/s²

1

Forward acceleration

44

131

4

AR

m/s²

1

Rightward acceleration

45

135

4

heave

m

1

Relative heave displacement

46

139

4

Filtered output

na

1

 

47

143

4

Filtered input

na

1

 

48

147

4

Main frequency

na

1

 

49

151

4

Integer part of the data time

-

-

 

50

155

4

Fractional part of the data time

-

-

 

51

159

4

Reserved

-

1

 

52

163

1

Checksum

Low 8 bits of the sum of the data length and the data bytes

1

 


Protocol 2: IMU Protocol

The backup IMU protocol outputs IMU data by default in timed broadcast mode. Each frame contains 40 bytes of data, the default output frequency is 200Hz, the baud rate is 115200bps, with 1 start bit, 8 data bits, 1 stop bit, and no parity.The data transmission uses a little-endian format with the low byte first. The baud rate and output frequency of the communication protocol can be configured.

Table4General IMU Protocol

Serial No.

Byte start index

Number of bytes

Content

Equivalent

Range

Unit

Remark

1

0

1

0x55

1

   

Frame header

2

1

1

0xAA

1

   

Frame header

3

2

1

36

1

   

Data length

4

3

4

PCnum

1

   

1 ms count value

5

7

4

Angular rate X

0.000001

[-2000,2000]

/s

 

6

11

4

Angular rate Y

0.000001

[-2000,2000]

/s

 

7

15

4

Angular rate Z

0.000001

[-2000,2000]

/s

 

8

19

4

Acceleration X

0.000001

[-40,40]

m/s²

 

9

23

4

Acceleration Y

0.000001

[-40,40]

m/s²

 

10

27

4

Acceleration Z

0.000001

[-40,40]

m/s²

 

11

31

2

System temperature

0.008

[-120,120]

℃

 

12

33

2

Year Month Day

-

-

-

Bit0~bit4: day 0-31

Bit5~bit8: month 0~12

Bit9~bit15: year 0~99

For example, 1100011110011111

represents December 31, 2099

13

35

4

Timestamp

0.1

-

ms

(h*3600+m*60+s)*10000

Example: 110011011111111001011111111111

Represents: 23h59min59.9999s

14

39

1

Checksum

1

[0,255]

 

Low 8 bits of the cumulative sum of bytes at indices (2–38)

 

GNSS Protocol

GNSS receiver configuration parameter list:

mode rover

CONFIG HEADING FIXLENGTH

CONFIG PPS ENABLE2 GPS POSITIVE 1000 1000 0 0

config com1 115200 n 1

config com2 460800 8 n 1

config com3 460800 8 n 1

GPGGA COM1 1

RANGECMPB com1 1

BD2EPHEMB com1 290

GPSEPHEMB com1 300

BESTPOSB COM1 1

KSXT COM2 0.1

GPGGA COM2 0.1

GPGGA COM3 1

RANGECMPB com3 1

BD2EPHEMB com3 290

GPSEPHEMB com3 300

BESTPOSB COM3 0.2

 

Inside the GNSS receiver:

The receiver COM1 port is an external output port, which can receive differential corrections and store differential data;

The receiver COM2 is the internal solution port;

The receiver COM3 port is the stored data output port, and the stored GNSS files can be decoded using GINS or decoded using the official decoding software from Unicore.

Decode it into RINEX-format data of version 3.02 or above for post-processing.

If you need the receiver to configure other types of output, please refer to Unicore Reference Commands Manual For N4 High Precision Products_V2_CH_R1.4.

 

Product precautions

  • Pay attention to the product electrical interface definitions. When using it, strictly follow the pin arrangement to avoid incorrect connections;
  • The product is a precision measuring device. During operation, be careful to avoid shocks, collisions, and other conditions beyond the product's tolerance range;
  • The installation of the product has a great impact on angular velocity measurement. To avoid introducing installation errors, the mounting surface is required to have good flatness;
  • To ensure measurement accuracy, the product must be installed firmly and reliably to avoid measurement errors caused by loosening;
  • When installing and using the product, attention should be paid to electrostatic protection; wearing an antistatic wrist strap is recommended;
  • Please operate strictly in accordance with the requirements of this manual, and confirm that the external environment is consistent with the usage requirements. If a problem occurs, do not disassemble the product cover or alter the internal structure of the product. If there is any issue, please contact and communicate with our technical personnel in a timely manner.

 

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