DLR Portal
Home
|
Textversion
|
Imprint
|
Sitemap
|
Contact
|
Deutsch
You are here:
Home
:
System Technology
:
Navigation and Control Systems
:
Test Facilities
Advanced Search
Institute
News
System Analysis
System Technology
Exploration Systems
Navigation and Control Systems
Satellite Formation Flying
Integrated Navigation Systems for Space Applications
Terrain based Navigation for Exploration Missions
Verification of Navigation and Control Systems
Simulation of Orbit and Position Control Systems
Projects
Test Facilities
Software
System Conditioning
Transport and Propulsion Systems
Avionics Systems
Projects
Facilities
Vacancies
Institute Seminar
Products
Navigations- und Regelungssysteme - Anlagen
Back
Send article to a friend
Print
GPS/INS Test and Verification Facility
GPS/INS Test and Verification Facility
.
The inner rotational axe in the climate chamber
.
Rotary table ACUTRONIC AC3347
Inertial sensors (rotational speed and acceleration sensors) are – on their own or in combination – the basis of many navigation systems. Before implementing such measurement devices it is necessary to test the functionality and quality of the sensor technology when combined with the entire navigation system. The GPS/INS facility was set up at DLR Bremen in 2009 to test and verify in-house devices. The facility is also available for external users and a DIN ISO certification is being prepared.
The facility consists of a Spirent GSS7700 GPS-simulator connected to an ACUTRONIC AC3347 rotation table to test GPS-supported inertial navigation systems, as well as other precision measurement devices for 3D coordinate evaluation and optical direction measurement.
The rotation table stimulates inertial sensors which can be calibrated by setting profiles of rotational speed. An integrated thermal chamber allows testing under defined temperature conditions and verification of temperature dependences in the sensor technology.
In addition to 30 electrical supply and signal lines, the rotation table’s inner platform offers a port for the GPS-antenna signal, provided via the GPS-simulator. Using the real time capable data interface SCRAMNet+ via a dSPACE-system, the rotation table can be embedded into hardware-in-the-loop testing.
Possible Services
Inner calibration of rotational speed sensors within a thermal chamber, determination of offset, scale factor, noise, drift, rotational speed limits, dynamic and their temperature dependence
Alignment measurements between several rotational speed sensors or for optical / mechanical references (case or mirror)
Testing and calibrating of GPS-receivers
Flight path simulation for rotational speed sensors and GPS-receivers using pre-set trajectories
Hardware-in-the-loop tests via a real time capable dSPACE-system
Thermal testing between -50°C and +80°C
Calibration of angle and inclination of the measurement system
GPS-Simulator Spirent GSS 7700
4-32 channels
GPS L1 supports C/A + P Code + M-Noise
GPS L2 supports C/A or p Code + L2C + M-Noise
GPS L5 supports L5 I and L5 Q
Complete flexibility through SimGEN software
Real time remote control and simulated flight path for hardware-in-the-loop
Output of different RF signal L1/L2
Interference of up to 16 channels on L1 band
Rotary Table ACUTRONIC AC3347
Continuing rotation around three axes with max. 1000°/s
Max. rotational speed acceleration between 400 and 30000°/s²
Orthogonality errors of each axis <3 arc seconds
Rotational speed solution 0.0001°/s
Temperature stabilization through climate chamber with CO2 cooling between -50°C and +80°C
Connection over SCRAMNet+ to the real time simulation platform dSPACE
450m diameter of inner rotary plate
15kg specific test object weight
GPS antenna line and other electric connections on the rotary plate
Contact
Michael Conradt
German Aerospace Center
Institute of Space Systems
Bremen
Tel.: +49 421 24420-1114
Fax: +49 421 24420-1120
Related Topics
Aircraft Communications and Navigation
Copyright © 2013 German Aerospace Center (DLR). All rights reserved.