Co-site Interference Testing of
VDL Mode 4 and AM-DSB Voice
Kim O'Neil
Advanced Aviation Technology Ltd.
Abstract
The introduction of new datalink services into civil
aviation is seen as one of the essential enabling technologies in the ICAO
CNS/ATM concept. Datalinks are required for new services such as Automatic
Dependent Surveillance - Broadcast (ADS-B) and Controller Pilot Data-Link
Communications (CPDLC), as well as improved airline operational communications
(AOC). These technologies will enable improvements in safety, capacity and
operational efficiency. Despite the obvious desirability of these services,
there is considerable debate about the merits of the various technologies on
offer. This paper is provided as information to airlines considering installing
ADS-B and datalink services based on ICAO's VDL mode 4 datalink.
1. Background
The datalink debate covers issues such as
functionality, performance, spectrum efficiency and aircraft integration and
has proven to be very contentious. Consequently, practical demonstrations of
datalink characteristics, have become a necessary requirement. VDL mode 4 has
already been subject to widespread trials across a very wide range of
operational applications. These trials have been extremely successful, and have
demonstrated the potential benefits of ADS-B, CPDLC and other CNS/ATM
applications. VDL mode 4 trials have involved many aircraft types, clocking up
more than a hundred and fifty thousand flight hours.
The aircraft trials and testing described here, were
carried out on a Boeing 737-600 to investigate any possible adjacent or
co-channel interference effects between VDLmode 4 and DSB-AM Voice in a
realistic operating environment, with radios operating in a typical
configuration. A realistic appraisal of radio quality was made in addition to
practical measurements. The trial was carried out by CNS Systems AB on an SAS B
737-600 test aircraft and were supervised by the Swedish CAA. Practical
demonstrations were made to an invited party of experts including ICAO AMCP
members and Eurocontrol participants. The full results and voice channel
recordings are available in a CD-ROM for comparison.
The tests demonstrate compliance to European Radio
Standards and successfully refute the somewhat surprising claims made by
proponents of other systems.
2. Available Datalink Technologies
Datalink technologies under consideration today
include: several VHF DataLinks (VDL), Satcom, Mode S and its variants and the
Universal Access Transceiver (UAT). For comparison purposes, these are
summarised:
2.1 VDL Mode 2
VDL mode 2 is an air/ground D8PSK datalink, nominally
operating at 31.5kbps, but with a net capacity estimated at around 3 to 4kbps.
VDL2 is a Carrier Sense Multiple Access (CSMA) link, consequently the link is
not available all the time - severely reducing its capacity. Significant
frequency planning is required to protect its channels - due to low frequency
re-use rates caused by high CCI (Co-Channel Interference) values of 22 - 26 dB.
Although nominally a 25kHz service, VDL2 requires adjacent channels to be
sterile. VDL 2 does not support tactical and time critical ATC datalink
requirements.
2.2 VDL Mode 3
VDL3 is a Time Division Multiple Access (TDMA) D8PSK
25kHz service, operating at 31.5 kbps, presumably synchronised to GPS time and
providing 4 channels per 25 KHz frequency (nominally 3 voice and 1 data). It
has the potential to provide wide area datalink services with data rates up to
12.4 kbps. Intended as a digital replacement for analogue VHF voice, it is a
key element of the FAA's planned ATC Nexcom upgrade.
2.3 VDL Mode 4
VDL4 is a Time Division Multiple Access (TDMA) GFSK
25 kHz service operating at 19.2 kbps with a net link capacity of 14kbps. VDL4
was specifically designed to be independent of ground infrastructure. It
permits any number of Users to simultaneously share the link, enabling both
air/air and air/ground communications. The FM modulation scheme also permits
frequency re-use, due to a low CCI value of 10dB - meaning the loudest (and
nearest) transmissions are always heard - and is consequently very spectrum
efficient. VDL4 has good range and capacity and is seen as a candidate for all
long-term applications. It has the greatest demonstrated capability in a wide
range of intensive studies across many aircraft types and ground ATM platforms.
2.3 Mode S Enhanced Surveillance
Mode S Enhanced Surveillance (EHS) consists of
Elementary Surveillance (ELS) with the addition of various Downlink Airborne
Parameters (DAPs). Although there are some overlaps, this technology does not
support air-to-air applications.
2.4 1090 Extended Squitter (ES)
1090ES is a derivative of Mode S technology, with
messages being squittered at a high rate. The channel is shared with SSR Mode
A/C, SSR mode S, Mode S EHS, TCAS/ACAS and military datalinks. The air-to-air
range of 1090ES is relatively poor, making it unsuitable for long-term purposes
and it suffers from multi-path (e.g. reflections from buildings, aircraft
etc.), also making it unsuitable for airport applications. This is well
documented in independent simulations and trials. 1090ES will saturate in
Europe around 2010. There are also concerns about overloading 1090MHz (also
occupied by TCAS) with yet another application.
2.5 Universal Access Transceiver (UAT)
UAT was developed by Mitre Corporation, and is a
random squitter broadcast technology operating at around 960MHz with a
bandwidth of 2-3MHz. Two message types are supported: air/air and air/ground
ADS-B messages and ground-station uplink messages (weather, Flight Information
Services - Broadcast FIS-B). This technology is a direct competitor to 1090 ES,
but has better range and capacity. Work on ICAO UAT SARPs will start in the
near future. Finding and protecting spectrum for UAT may be difficult.
| Link Technology |
Air/Ground COM |
Air/Air COM |
Air-Air Broadcast |
Uplink Broadcast |
Downlink Broadcast |
| Avpac/Acars |
Y |
|
|
|
|
| HFDL |
Y |
|
|
|
|
| AMSS |
Y |
|
|
|
|
| 1090 ES |
|
|
Y |
Y |
Y |
| Mode S ES |
|
|
|
Y |
Y |
| VDL2 |
Y |
|
|
Y |
|
| VDL3 |
Y |
|
|
Y |
|
| VDL4 |
Y |
Y |
Y |
Y |
Y |
| UAT |
|
|
Y |
Y |
Y |
Table 1: Comparison of Datalink Functionality 3. VDL
Mode 4 to AM-DSB Voice Test
Objectives
The purpose of the test was to investigate the
potential for co-site interference between a VHF Datalink Mode 4 radio
operating (i.e. transmitting ADS-B messages) simultaneously with a AM-DSB voice
radio onboard the same airframe. The tests investigate possible co-channel and
adjacent channel interference of VDL 4 datalink to VHF Voice. Necessarily,
protection of voice channels is an absolute primary safety concern.
4. Test set-up
The operational test was carried out at Linkoping
Airport in Sweden in May 2003, using an SAS Boeing 737-600 aircraft. The VDL
mode 4 Transponder Unit was manufactured by CNS Systems. The test was
supervised by the Swedish Civil Aviation Administration (LFV) and carried out
by CNS Systems AB, with the cooperation of SAS.
5. Hardware
Table 2 summarises the hardware configuration employed
in the test, whilst Table 3 details the specific frequency test set up.
| Unit |
Manufacturer |
Part Number |
Serial No |
| VHF COM 1 |
Rockwell Collins |
822-1047-003 |
3958 |
| VHF COM 2 |
Rockwell Collins |
822-1047-003 |
6969 |
VDL 4000/GA VDL Mode 4 Transponder
to VHF antenna COM 3 |
C.N.S. Systems |
4000-10-10 |
1025 |
| Handheld VHF voice radio |
ICOM |
|
|
| VHF antenna COM 1 |
Ail System Inc. |
DMC50-17 |
14964 |
| VHF antenna COM 2 |
Ail System Inc. |
DMC50-17 |
13054 |
| VHF antenna COM 3 |
Ail System Inc. |
DMC50-17 |
14346 |
| SAS Aircraft B737-600 |
Boeing Aircraft |
Reg. LN-RRZ |
28295 |
Table 2: Hardware Configuration
6. Setup
| Unit |
Antenna |
Frequency |
Usage |
| VDL Mode 4 Transponder
|
COM3 |
Constant: 136.950 MHz |
Interferer transmitter |
| Handheld VHF voice radio
|
Integrated |
136.700 to 136.950 MHz1 |
Wanted transmitter |
| VHF radio 1 |
COM1 |
136.700 to 136.950 MHz1 |
Victim receiver |
| VHF radio 2 |
COM2 |
Constant: 136.950 MHz |
Victim receiver |
Table 3: Test Set up
Note that frequencies normally interfering with the
regular air traffic were not used. The interfering transmitter was the co-site
VDL Mode 4 transponder transmitting ADS-B data at the specified frequency. The
load was 13.3 ms bursts at 1 Hz repetition rate.
PICTURE HERE Figure 1: Illustration of Test
Scenario.
7. Test Results
A qualitative analysis of interference from VDL Mode 4
transmitter to VHF radio 1 victim during voice communication, gives the
following results:
Frequency AM-DSB (MHz) |
Range
TX/RX AM-DSB (m) |
Audible
Interference(Y/N) |
| 130.9501 |
5 |
N |
| 136.700 |
15 |
N |
| 136.725 |
15 |
N |
| 136.750 |
15 |
N |
| 136.775 |
15 |
N |
| 136.800 |
15 |
N |
| 136.825 |
15 |
N |
| 136.850 |
15 |
N |
| 136.875 |
15 |
N |
| 136.900 |
15 |
N |
| 136.925 |
15 |
N |
| 136.950 |
15 |
Y (This is the co-channel) |
| 130.950 |
200 |
N |
| 136.700 |
200 |
N |
| 136.725 |
200 |
N |
| 136.750 |
200 |
N |
| 136.775 |
200 |
N |
| 136.800 |
200 |
N |
| 136.825 |
200 |
N |
| 136.850 |
200 |
N |
| 136.875 |
200 |
N |
| 136.900 |
200 |
N |
| 136.925 |
200 |
N |
| 136.950 |
200 |
Y This is the co-channel) |
Table 4: Analysis of Impact of VDL 4 on VHF Voice
Recordings and analysis of the voice channel supports
the results of Table 4. Recordings of the voice channels are available on a
CD-ROM for independent analysis.
8. Analysis of Potential Interference
Analysis of potential interference from VDL Mode 4
transmitter to AM-DSB victim during voice communication is recorded in Table 5:
| VDL Mode 4
interferer |
| Output power, TX port |
40 dBm |
Transponder setting |
| Cable loss |
1 dB RG58, 5m, |
Assumed |
| Antenna gain, COM3 |
0 dB |
Assumed |
| TX power at COM3 antenna |
39 dBm |
Pt - Loss |
| Isolation COM1 - COM3 |
48 dB |
See VM4AAS D3.2 p85. Small
aircraft, opposite side antennas. |
| RX power at COM1 antenna |
-9 dBm |
Pt - Iso |
| AM-DSB Wanted
Signal |
| Output power,TX port |
32 dBm |
Transmitter spec. 1.6W |
| Antenna gain |
0 dB |
Assumed |
| TX power at antenna |
32 dBm |
@nbsp |
| Space loss, R=15 m / R=200m |
38.6 / 61.1 dB |
20log10(4?R/?) |
| RX power at COM1 antenna |
-6.6/-29.1 dBm |
Pt - SL |
| AM-DSB Received
Signals |
| Signal-to-Interferer at RX
input |
2.4 / -20.1 dB |
|
Signal-to-Interferer at demod
input, co-channel (0 kHz offset) |
2.4 / -20.1 dB |
Audible interference |
| ACR @ 25 kHz > |
60 dB |
Assume ACR as ARINC716-10 |
| Signal-to-Interferer at demod
input, adjacent channel (25 kHz offset) |
>62.4 / 39.9 dB |
No audible interference |
| Signal-to-Interferer at demod
input, Acceptable limit |
12 dB |
See VM4AAS D3.2
p86. Signal-to-Pulse ratio required for voice/VDL Mode 4. |
Table 5: Analysis of VDL4 interference into AM-DSB
Voice VDL Mode 4
| Interferer Output
power |
| TX port |
40 dBm |
Transponder setting |
| Cable loss |
1 dB |
RG58, 5m, assumed |
| Antenna gain, COM3 |
0 dB |
Assumed |
| TX power at COM3 antenna |
39 dBm |
Pt - Loss |
| Isolation COM2 - COM3 |
22 dB |
VM4 AAS D3.2 p85 Small
aircraft, same side antennas |
| RX power at COM2 antenna |
+17 dBm |
Pt - Iso |
Table 6: VDL Mode 4 TX interference to AM-DSB
victim on idle voice channel.
The AM-DSB receiver must be saturated at this high
input level. However, the squelch did not open in any case.
9. Results
The results of the live test are consistent with the
calculations indicated above. Audible ADS-B transmissions were only present in
the co-channel case when the S/P value was much worse than the required 12 dB.
Even with -20 dB S/P (as calculated above) the audible clicks from ADS-B
transmissions with 1 Hz rate were quite acceptable and did not adversely affect
voice communications. There was no audible interference on the first adjacent
channel or at further channel separations. This is expected, since the radio
should have ACR 60 dB @ +/- 17 kHz according to the ARINC 716-10 standard, and
even better ACR at 25 kHz and larger offsets.
The test set-up and original results are documented
on video, pictures and in audio files. A CD with the complete material can be
obtained from kim.oneil@aatl.net or
fredrik.lindblom@lfv.se
10. Conclusions
There was no audible interference on any of the
adjacent channels - whether or not the squelch was open or closed. At the
co-channel with the squelch closed, no ADS-B transmissions could be heard.
Significantly, the squelch was not opened by the ADS-B transmissions. With the
squelch open, the ADS-B transmissions could be heard as very short clicking
sounds. The voice test message being read on the same channel was still heard
loud and clear. Any reasonable aircraft installation should provide excellent
and well-behaved VDL mode 4 datalink performance with no adverse impact on
voice communications on any of the voice channels. This well-behaved
performance is consistent with the practical experience gained in the many VDL
mode 4 trials carried out on many different aircraft platforms. |