Radio propagation: Difference between revisions

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If you are involved with maintenance or have detailed information about navaid transmitter capabilities, the author would appreciate if you listed in the discussion page the following information:
If you are involved with maintenance or have detailed information about navaid transmitter capabilities, the author would appreciate if you listed in the discussion page the following information:


* usual transmitter power for localizer (known to be between 15-25 W) and glideslope (known to be between 5-10 W) equipment.
* usual transmitter power for localizer (known to be between 15-25 W) and glideslope (known to be between 5-10 W ???) equipment.
* usual transmitter power for DME (not VOR) equipment.
* usual transmitter power for DME (not VOR) equipment: various source suggest from 50 W to 1 kW (!!??).
* usual antenna types and gains for localizer and glideslope equipment (for localizer the ERP is known from various sources as approx 100 W, thus assuming 7-9 dBi antenna gain).
* usual antenna types and gains for localizer and glideslope equipment: for localizer the ERP (effective radiated power) is known from various sources as approx 100 W, thus assuming 7-9 dBi antenna gain, glideslope antenna estimated gain 10 dBi <ref>http://www.dbsant.com/gsSpecs.php</ref>.
* usual localizer/glideslope antenna types and gains for various aircraft, for usage by aircraft developers.
* usual localizer/glideslope antenna types and gains for various aircraft, for usage by aircraft developers.



Revision as of 22:03, 26 November 2012

Summary

The code and algorithms described below enable the following features in Flightgear, which to the author's knowledge are unique for a conventional flight simulator:

  • realistic radio reception of ATC and AI aircraft messages.
  • realistic radio reception of VOR stations, making radio navigation more interesting and realistic in hilly/mountainous terrain.
  • mostly realistic radio reception of localizer and glideslope signals, making landings more interesting for certain airports.
  • configuration and realistic reception of radio beacons located anywhere in the 3D world, while presenting calculated signal values according to different official guidelines, including but not limited to the FAA.


Using Flightgear as a general purpose, 3D, radio signal propagation and terrain analysis tool

The purpose of this document is to evaluate the possible usage of the Flightgear engine as a tool for RF signal loss prediction over a rough terrain, using geographical features embedded inside terrain data and well know propagation prediction algorithms.


There are currently a number of freeware and open-source applications that perform RF signal loss analysis using data available to the general public (elevation data, landcover etc.). Well known and used are Radiomobile [1], a Windows application by Roger Coudé, VE2DBE and Splat![2] (multiple platform) by John A. Magliacane, KD2BD.


A common point of these applications is the usage of the Irregular Terrain Model (also known as Longley-Rice) which is a propagation model developed by the U.S. Department of Commerce NTIA/ITS - Institute for Telecommunication Sciences and improved by several others (notably ITWOM [3] by Sidney E. Shumate, code available to the public on a limited usage license, copyright Givens-Bell [4]).

It is a general purpose model that can be applied to a large variety of engineering problems. The model, which is based on electromagnetic theory and on statistical analysis of both terrain features and radio measurements, predicts the median attenuation of a radio signal as a function of distance and the variability of the signal in time and in space.[5] It is currently used among others by NASA, Alcatel-Lucent, US Army, University of Massachusetts and amateur radio operators around the world, and is widely considered the best propagation model for frequencies between 50 - 5000 Mhz freely available to the public.

Rationale

Radio signal analysis
Antenna far-field gain plot

The implementation of radio propagation analysis is mostly finished inside Flightgear. Since the terrain used by this open-source flight simulator contains both elevation information and landcover data, it seems especially suited for a 3D tool to predict RF signal levels, both for aviation navigational aids and radio communications, and standalone as a point-to-point radio link analysis between two radio stations. Flightgear allows the user to place models on the terrain at specific locations, and to setup internal properties via a simple XML format. Rather complex radio receivers and transmitters can be simulated using the Nasal scripting language or via an external utility, as well as an UI to perform signal level reading and modify receiver and transmitter physical characteristics. The 3D aspect is also interesting, since it allows one to perform predicted signal level reading at different locations while inside the simulator, using visual cues to place the radio equipment on the terrain. Since this open-source flight simulator is capable of running on multiple platforms, including GNU/Linux, Microsoft Windows and MacOS, its availability is not limited to one operating system.

Data

Most of new generation Flightgear terrain uses NASA SRTM v3 [6] elevation data, which has a distance of 90 meters between elevation points. This is considered accurate enough for most signal analysis, although more detailed elevation data from topographical maps, ASTER DEM or other sources can be acquired. Default landcover in Flightgear comes from VMAP0 [7] layers, with more accurate geodata being available from national and international programs, such as Europe's flagship program, the CLC2006 "Corine" landcover project.[8] Landcover data is used to analyse path loss and improve predicted signal levels over specific types of terrain, but should be cross-checked with real-world RF signal readings took at the same locations. Antenna radiation patterns obtained using the free tool NEC2x can be used for both transmitters and receivers. Patterns obtained from other applications can be used too, as long as they are converte to the rather simple text format which is used by the Flightgear radio code. Also, data from Flightgear's realistic atmospheric and weather simulation could be taken into account when path loss analysis is perfomed.

Request for information

If you are involved with maintenance or have detailed information about navaid transmitter capabilities, the author would appreciate if you listed in the discussion page the following information:

  • usual transmitter power for localizer (known to be between 15-25 W) and glideslope (known to be between 5-10 W ???) equipment.
  • usual transmitter power for DME (not VOR) equipment: various source suggest from 50 W to 1 kW (!!??).
  • usual antenna types and gains for localizer and glideslope equipment: for localizer the ERP (effective radiated power) is known from various sources as approx 100 W, thus assuming 7-9 dBi antenna gain, glideslope antenna estimated gain 10 dBi [9].
  • usual localizer/glideslope antenna types and gains for various aircraft, for usage by aircraft developers.

Implementation details

In order to use the point-to-point routine of the Longley-Rice model, a terrain profile between the two radio stations is generated by sampling the terrain with a configurable distance between points (default is 90 meters, which is equal to SRTM 3 arcsec precision). This terrain profile is fed to the ITM routines, together with some other parameters: transmitter output power, receiver sensitivity, antenna heights above terrain. These routines are the core of the implementation, and incorporate improvements made by J. D. McDonald, John A. Magliacane and Holger Schurig to the original code.

The result is signal attenuation in dB along the direct path. The ITM functions will determine for us if the radio propagation is line-of-sight, diffraction dominant or tropospheric scatter. For diffraction propagation, it also determines if it's single horizon or double horizon. This information will further be used in calculating ground clutter obstruction for different terrain types. The most frequent obstructions that affect radio signals are built-up areas and tall vegetation. By calculating the interference of ground clutter inside the first Fresnel zone, we can determine signal losses with average precision. In order to do so, we need two more factors in the equations: clutter height above terrain, and clutter density. These could be stored in the material database in the future, but are hardcoded for now, at least for a number of terrain types. The aim is to make these two factors as configurable as possible to the user, in order to be able to adapt them to local measured conditions.

The radio stations parameters are also completely configurable by the user, by setting internal properties, via Nasal scripting or otherwise. For ATC comms, at the current state, some basic assumptions are made about transmitter power, receiver sensitivity and antenna heights: these are based on standard ATC interactions, but this will be changed in the future to support a wider variety of signals. It might even be possible to simulate realistic ACARS transmissions, as well as transponder responses with realistic range and signal quality (introduce errors based on signal quality etc.)


Known limitations

  • The loading distance of terrain. For stations which are beyond the maximum configured terrain loading distance, path profiles will not be accurate and some errors are likely to occur in the signal loss figures.
  • The current model does not take into account signal reflection from objects or terrain features, nor refraction caused by atmospheric conditions.
  • The diffraction calculations within the ITM library are not very precise and are likely to overestimate losses caused by diffraction over a sharp edge, or when take-off angles are beyond a certain limit. This has been corrected in the new ITWOM, which is available to the public with commercial restrictions. [10]
  • Clutter loss calculation are only estimative and should only be taken into account after careful calibration done with measurement equipment at the sites.

Currently implemented features within the Flightgear engine

VOR received on ground 80 km away with no line of sight, using old code
VOR no longer received on ground 80 km away with no line of sight, using new radio code
  • the code has been transitioned to a more efficient and performance-friendly subsystem structure
  • point-to-point path loss calculations over rough terrain using the ITM library for air traffic control stations to pilot communication. Also AI to pilot reception.
  • point-to-point path loss calculations using the ITM library for VOR/Localizer and Glideslope stations [11].
  • for VHF/UHF stations beyond a reasonable terrain loading distance, automatic transition to path loss calculation over a smooth round earth using alternative free space signal attenuation equations
  • RF link budget calculations using transmitter power, receiver sensitivity, antenna gain and height above terrain, taking into account typical values from various specifications
  • experimental feature: usage of detailed landcover in RF propagation prediction (ground clutter path loss)
  • signal loss due to polarization mismatch
  • simple signal strength indicator (Instrument for signal level reading)
  • far-field antenna radiation patterns generated with 4nec2
  • placing a radio transmitter beacon with the model tool inside 3D space
  • using the property tree, a radio station can be defined with Nasal scripts
  • support for multiple radio stations running at the same time: navaids, ATC comms, beacons
  • efficiency mode: the number of terrain data points decrease proportionally with the distance to the station.
  • calculation of electrical field strength in uV/m, received signal strength in uV and dBm, as required by official guidelines.

Features which still need to be implemented

  • separate DME from VOR reception, since it uses a completly different range of frequencies: in reality, when VOR-DME directional signal is received, it is possible that DME information is not available, due to terrain/weather or ground clutter influence. [12]
  • reception of ACARS ground messages via VHF radios
  • usage of weather simulation and atmospheric conditions which affect radio propagation: tropospheric ducting, cloud backscatter etc.
  • simulate realistic transponder response
  • realistic ground-to-air radar

Mailing list discussions


References