2 interface board, 3 antenna – Mitel GPS Orion-S/-HD Receiver User Manual

Page 11

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Document Title:

7

User’s Manual for the GPS Orion-S/-HD Receiver

Document No.

Issue 1.0

GTN-MAN-0110

June 22, 2003

DLR/GSOCNo part of this document shall be reproduced in any form or disclosed to third parties without prior authorization.

2.2 Interface Board

The interface board provides auxiliary devices that are required for standalone operation of
the Orion receivers. It comprises

a switching regulator allowing operation from unregulated power supplies,

a rechargeable battery to maintain the non-volatile memory and real-time clock during
power down times and

two RS232 serial line drivers for communication with standard peripheral devices.

Key parameters of the interface board are summarized in Table 2.2.

Table 2.2 Physical and electrical parameters of GPS Orion interface board

Parameter

Value

Dimension

95mm x 50mm x 20mm

Weight

70g

Operating voltage

8–30V

Efficiency of switching regulator

85%

Total power consumption (I/F and main board) 2.4 W
Battery

+3.6V NiCad, 110 mAh ([1])

I/O ports

2 x RS232 (±10V)
Sub-D9 connector (male)


The two serial ports support the ground, receive and transmit line using the standard pin as-
signment for Sub-D9 connectors (Table 2.2). Pins 7 and 8 are cross-connected since the
Orion receiver does not support a hardware handshake. Likewise the three pins 1, 4, and 6
are connected among each other.

Table 2.2 Pin assignment for RS232 Sub-D9 connectors (Port A and B)

Pin

Description

Remarks

Schematic

1

DCD (Data Channel Received
Line Signal Dete ctor)

Connected with DTR and DSR (pins 4 , 6)

2

RxD (Receive Data)

3

TxD (Transmit Data)

4

DTR (Data Terminal Ready)

Connected with DCD and DSR (pins 1 , 6)

5

GND (Signal Ground)

6

DSR (Data Set Ready)

Connected with DCD and DTR (pins 1 , 4)

7

RTS (Request to Send )

Connected with CTS (pin 8)

8

CTS (Clear to Send)

Connected with RTS (pin 7)

9

RI (Ring Indicator)

Not connected

2.3 Antenna

The GPS Orion receiver is operated with an active antenna (or a passive antenna and exter-
nal preamplifier) having a minimum gain of 16 dB and a noise-figure of less than 4 dB More
specifically, the ANPC-131 antenna of M/A COM is recommended (cf. [4]), for terrestrial ap-
plications. It offers an LNA gain of +26 dB and a 1.5 dB noise-figure at the L1 frequency
(1575.42 MHz).

For space applications dedicated antenna designs with heat and vacuum resistant radomes
are generally required. For sounding rockets wrap around antennas, helix tip antennas or
blade antennas with separate preamplifiers are available on request. GPS antennas for
satellite applications are offered by e.g. Sensor Systems Inc.

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