Beijing Oriental Lianxing Technology Co., Ltd
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    7th Floor, East Area, Building 4, Shangdi Science and Technology Building, No. 8 Shangdi West Road, Haidian District, Beijing
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TOAS100D Dual Antenna Satellite Direction Finding System
TOAS100D Dual Antenna Satellite Direction Finding System
Product details

The TOAS100D dual antenna direction finding system is a miniaturized dual antenna direction finding system based on the latest multi RF unit synchronization technology from Eastern Union. The system adopts more precise carrier phase relative positioning differential technology, thereby achieving high-precision and high stability heading measurement in both static and dynamic situations. The GPS measurement unit of the TOAS100D dual antenna direction finding system simultaneously receives dual GPS satellite signals through dual antennas. By effectively combining the carrier phase observations of dual GPS channels, it can achieve heading accuracy of up to 0.1 degrees (2M) with high measurement reliability, and the directional results do not drift over time. Suitable for navigation, positioning, speed measurement, orientation, and precise timing of various aircraft, vehicles, ships, and other moving carriers.


characteristic

Dual channel satellite signal synchronization technology - using independently developed baseband chips to achieve real-time synchronization and high-precision observation data sampling of dual channel antennas.

Carrier smoothing code phase relative difference technology - realizes high-precision, high stability, and anti multipath interference heading measurement in both static and dynamic situations.

Integrity monitoring - a technology that uses multiple redundant measurement values to monitor the integrity and eliminate gross errors of each channel of satellite navigation chips, improving the reliability of satellite navigation unit operation.


application
Aviation navigation and orientation;
Vehicle navigation, positioning and orientation;
From ship navigation and orientation;
Direction finding, north finding, and timing;
Unmanned aerial vehicle navigation control.


Output Content
Heading and pitching
Three dimensional position (longitude, latitude, altitude)
Three dimensional velocity (eastward velocity, northward velocity, celestial velocity)
Accurate Time (UTC)



TOAS100D Technical Specifications

Attitude accuracy

Heading angle

0.1 ° (1 σ) (baseline 2m)

Pitch angle

0.2°(1σ)

Accuracy index

Horizontal position accuracy

5.0m(1σ)

Uniform speed measurement accuracy

0.05m/s(1σ)

Variable speed measurement accuracy

0.10m/s(1σ)

1PPSoutput

±100ns

Time indicator

Re capture time

<>s

Hot start time

1s

Cold start time

35s

First heading lock time

<>

Output Content

navigation data

Specialized binary format (position, velocity, attitude, time)

raw data

Satellite raw channel data

Effective bandwidth

>50Hz

Angular velocity range

±90°/s

Input output interface

antenna interface

SMA (2 pieces)

Digital Interface

Y34QM-19

output interface

RS232/RS422

Data update rate

1Hz

INPUT VOLTAGE

9V~36VDC

power consumption

2W@12VDC

Electrical characteristics

Anti vibration

8g(20 Hz~2000 Hz)

Impact resistance

1000g(10ms)

physical property

operation temperature

-40 ℃ to+75 ℃

storage temperature

-55°Cto +85°C

size

186.4×138×69.5mm

weight

1100 g (shell) 90 g (single board)

Note: Items such as update rate, positioning method, second pulse, and output content in the table all have different levels of output, and users can choose according to their actual application needs.

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