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PS11129BENAC01

TDM880i - Instruction Manual

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This document is the property of Airbus DS SLC and should not be copied or circulated without permission.

DECLARATION OF CONFORMITY We, Airbus Defence and Space Oy, Hiomotie 32, 00380 
Helsinki, Finland, declare under our sole responsibility that the product TDM880i is in 
conformity with the provisions of the following Council Directives: 

• 2011/65/EC (ROHS). 
• 2014/53/EU (Radio Equipment Directive).

Copies of the Declaration of Conformity can be found at https://cinfodin-airbusds.com

When installed or integrated as a part of another electrical device or interfaced with an external device, the 
integrator or manufacturer of the aforesaid device or assembly (’the End Product Manufacturer/System Integrator’) 
is responsible for compliance with all applicable local and other regulations, including but not limited to EMC, SAR 
and safety regulations, and must obtain all necessary approvals and permits concerning the final device or 
assembly. 

The above mentioned Declaration of Conformity by Airbus Defence and Space Oy concerns the TDM880i as a 
standalone product. The End Product Manufacturer/System Integrator has the responsibility of providing separate 
Declaration of Conformity concerning the whole system/application to which TDM880i is installed.

Airbus Defence and Space Oy disclaims any and all liabilities in respect of the aforesaid.

Copyright © 2015-2017 Airbus DS SLC. All rights reserved.

Airbus Defence and Space® is a registered trademark of Airbus Defence and Space. Other product names, 
trademarks or other identifiers mentioned in the document may be trademarks of their respective companies and 
are mentioned for information purposes only.

The document is confidential and contains legally privileged information. The document may only be used for the 
purpose for which it is submitted. Reproduction, transfer, distribution or storage of part or all of the contents in this 
document in any form without the prior written permission of Airbus Defence and Space is prohibited.

Airbus Defence and Space operates a policy of continuous development. Airbus Defence and Space reserves the 
right to make changes and improvements to any of the products described in this document, and the right to revise 
this document or withdraw it at any time without prior notice.

Airbus Defence and Space will reasonably ensure that the information provided in this document is free from 
material errors and omissions. However, the suggestions, directions, comments and statements made in the 
document (e.g. regarding the compatibility, performance and functionality of mentioned hardware and software) 
are not intended to be and cannot be considered as binding. The contents of this document are provided "AS IS". 
The customer assumes full responsibility for using the document or any part of it. All comments and feedback are 
welcomed by Airbus Defence and Space and are used as part of the continuous development and improvement of 
Airbus Defence and Space’s products, services and the document. Except as required by applicable law, no 
warranties of any kind, either express or implied, including, but not limited to, the implied warranties of 
merchantability and fitness for a particular purpose, are made in relation to the accuracy, reliability or contents of 
this document.

To the maximum extent permitted by the applicable law, under no circumstances shall Airbus Defence and Space 
be responsible for any loss of data or income or any special, incidental, consequential or indirect damages 
howsoever caused.

The availability of particular products may vary by region. Please check with the Airbus Defence and Space 
reseller nearest to you.

The use and operation of this device is subject to permission: for details contact your local frequency authority.

Includes RSA BSAFE cryptographic or security protocol software from RSA Security.

The crossed-out wheeled bin means that within the European Union the product must be taken to separate 
collection at the product end-of-life. This applies to your device but also to any enhancements marked with 
this symbol. Do not dispose of these products as unsorted municipal waste. Please deliver this product after 
operational life to your distributor or sales representative for recycling.

Summary of Contents for TDM880i

Page 1: ...PS11129BENAC01 06 2017 TDM880i Instruction Manual...

Page 2: ...rbus Defence and Space operates a policy of continuous development Airbus Defence and Space reserves the right to make changes and improvements to any of the products described in this document and th...

Page 3: ...types making of cables 12 Installation procedure 13 Installing the TDM880i 13 Powering up considerations 14 Connecting the power supply 14 Cabling 14 Connecting the power supply 14 Special considerati...

Page 4: ...ission TETRA Terminal Programming Tool TPT 24 AT interface 25 SDS interface 25 Alerting feature 26 TETRA Terminal Programming Tool TPT 26 AT interface 28 SDS interface 28 IGS feature 29 7 CONNECTOR IN...

Page 5: ...very endeavour has been made to ensure the accuracy of this document some errors may exist If any errors are found by the reader Airbus Defence and Space Oy should be notified in writing Please state...

Page 6: ...s with AIMD should keep the radio at least 20 cm 7 9 in away from the AIMD device If you have any reason to suspect that interference is taking place switch off your radio immediately and contact the...

Page 7: ...will corrode electronic circuits Do not use or store the radio in dusty dirty areas Its moving parts can be damaged Do not store the radio in hot areas High temperatures can shorten the life of elect...

Page 8: ...vides a set of digital I O lines that can be configured as inputs or outputs The outputs can be controlled by SDS messages the inputs can be used to trigger a status message or location sending to pre...

Page 9: ...nded for indoor use in weather protected dry conditions only The power supply is CE approved and conforms to EU EMC requirements DC Power Cable CA 124 The DC power cable CA 124 has a matching connecto...

Page 10: ...ithout permission Select the best suitable good quality antenna for the use case Airbus offers a selection of antennas for which you can find more information in the accessory catalogue Alternatively...

Page 11: ...certain fault conditions emitted RF energy may affect to operation of these systems If necessary consult the vehicle dealer manufacturer to determine the immunity of vehicle electronic systems to RF...

Page 12: ...ower supply to a battery or another DC supply so that the black wire is GND 0V the green wire is the IGS signal and the red wire is the VCC signal 10 6 16 0 V The maximum recommended length of the pow...

Page 13: ...onal accessory CA 126 is available in Airbus Defence and Space to convert from a MMBX to a TNC female GPS RF cable The connector of the TDM880i board is a 50 impedance matching IPX connector female Hi...

Page 14: ...connected to the radio module are fastened in a manner that does not cause bending twisting pushing pulling or vibrating in the connectors of the radio 11 Connect the power cable Set the IGS signal th...

Page 15: ...n from the body of the vehicle NOT directly from the battery Lightning protection Protect the antennas in particular from lightning using lightning rods surge arrestors gas discharge tubes and or othe...

Page 16: ...ct the DAU 9S cable to a COM port of a PC and then connect the DAU 9S with the CA 125 and radio module 3 Start the TETRA Terminal Programming Tool the version 2009 20 53 4 or later of TPT should be us...

Page 17: ...gnition and powering the radio ON OFF accordingly see Section Ignition sense IGS functionality on page 21 Tracking and positioning The TDM880i can be configured to send its location information period...

Page 18: ...il the correct time date are recovered After the successful retrieval of the correct time the Sleep mode functionality continues execution as configured Periodic reset Data terminals can be installed...

Page 19: ...power and runs out of backup power the main clock of the device resets In this case the Time Recovery sequence is started during the next startup See Section Time recovery on page 19 When the device h...

Page 20: ...03 and X102 connectors the levels of input and output signals are 5 V TTL excluding the FBUS and MBUS signal See Section CONNECTOR INTERFACES on page 31 In the CPU connector the inputs and outputs are...

Page 21: ...y The power on off is controlled in the TDM880i through an IGS input signal The signal is provided through multiple connectors with multiple voltage level variants To power up the TDM880i raise any of...

Page 22: ...message from a predefined SSI TETRA Terminal Programming Tool TPT The TPT can be used to configure the Sleep mode feature in two ways to configure the set of SSI from which the configuration SDS mess...

Page 23: ...Table 5 Sleep mode parametrization SDS interface After a new configuration is retrieved a special acknowledgement message is sent to the configuration sender The format of the acknowledgement is as f...

Page 24: ...d tracks the distance trigger expressed as meters Table 7 Location tracking parameters TETRA Terminal Programming Tool TPT The TPT can be used to configure the Location tracking feature in two ways to...

Page 25: ...etrization AT interface SDS interface Parametrization of the Tracking functionality over an SDS message requires that the message format presented below is used Table 9 Tracking parametrization SDS in...

Page 26: ...y to include alert statuses into LIP messaging Acknowledgement allowed from all numbers The alert specific parameters are IO line bound to alert Alert handling None SDS 1 or SDS 4 messaging when alert...

Page 27: ...are 32 individual alerts which can be configured using the shown dialog to Send a status message on alert Send an SDS 4 on alert Configure the message contents and destination address In addition to t...

Page 28: ...10 Allowed from all numbers 0011 Both enabled Sub block count 8 bits Number of sub blocks single block update supported currently Sub block ID 8 bits reserved Sub block size 8 bits reserved Message ty...

Page 29: ...e 13 Acknowledgement message format IGS feature The IGS feature can be configured using the Mobile Parameterisation view shown in Figure 8 Explanation of parametrization The Power Off Timer gives the...

Page 30: ...M 8 8 0 I S P E C I F I C P A R A M E T E R S PS11129BENAC01 TDM880i Instruction Manual 30 36 This document is the property of Airbus DS SLC and should not be copied or circulated without permission F...

Page 31: ...ut cable CA 124 must be fuse protected VCC 5A IGS 1A Use the wire size AWG 12 or larger It is recommended to connect all the power cable pins according to Table 14 Table 14 Power supply connector X104...

Page 32: ...supply 8 OVERTEMP out 2 78 V Over temperature indicator signal active high 9 MBUS in out 2 78 V MBUS serial line connect 560 pull down resistor to BSI line to switch MBUS from X901 to X103 requires r...

Page 33: ...out 5 V Max current 200mA see Note 2 NC Do not connect 3 GPS_FIX out TTL GPS fix indicator signal active high 4 GND gnd 0 V Ground 5 IN_SERVICE out TTL In service indicator signal active high 6 POWER...

Page 34: ...W typical average in addition to other power consumption when on Idle 960 mW typical average Sleep 864 mW typical average IGS in logic high state Shut down 3 6 mW typical average OPERATING TEMPERATURE...

Page 35: ...y of Airbus DS SLC and should not be copied or circulated without permission T E C H N I C A L D A T A The mechanical dimensions of the TDM880i illustrated in Figure 10 and Figure 11 Figure 10 TDM880i...

Page 36: ...obile Equipment GPS Global Positioning System GTS GPS Tracking Server IGS Ignition Sense I O Input output LED Light Emitting Diode LIP Location Information Protocol LNA Low Noise Amplifier MMBX Microm...

Page 37: ...TRA TR APP 00093 02 03 EN PS11129BENAC01...

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