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Specification for WAAS/EGNOS decoder module: - GetACoder

Specification for WAAS/EGNOS decoder module: - GetACoder

Specification for WAAS/EGNOS decoder module: - GetACoder

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<strong>Specification</strong> <strong>for</strong> <strong>WAAS</strong>/<strong>EGNOS</strong> <strong>decoder</strong> <strong>module</strong>:<br />

Introduction:<br />

The required software <strong>module</strong> will written in Visual Basic and accept in<strong>for</strong>mation in<br />

the <strong>for</strong>m of 250 bit data packets, at a rate of at least 1Hz, identify the message type<br />

and decode the contained in<strong>for</strong>mation appropriately, applying the extracted data if<br />

relevant to an internally stored database of recently received in<strong>for</strong>mation.<br />

The <strong>module</strong> will provide several functions (specified below) which apply this<br />

received and stored data to calculating positional corrections and accuracy<br />

in<strong>for</strong>mation <strong>for</strong> GPS satellites, and outputting this in<strong>for</strong>mation in suitable number<br />

<strong>for</strong>mats.<br />

The required equations and procedures, and the data <strong>for</strong>mats of the received packets<br />

are all fully specified in either:<br />

U.S. Department of Transportation ‘WIDE AREA AUGMENTATION SYSTEM<br />

(<strong>WAAS</strong>) [FAA-E-2892B, Change 1, DTFA01-96-C-00025 Modification No:0051]<br />

GLOBAL POSITIONING SYSTEM STANDARD POSITIONING SERVICE<br />

SIGNAL SPECIFICATION 2nd Edition June 2, 1995<br />

Both of which will be provided along with other documents of an explanatory or<br />

background nature.<br />

Of particular importance is the correct application of the ‘Issue of Data’ and ‘Time of<br />

applicability’ in<strong>for</strong>mation associated with the received data in ensuring only currently<br />

relevant in<strong>for</strong>mation is used.<br />

Most of the stored in<strong>for</strong>mation will be seconds or minutes old, and to calculate the<br />

corrections to the relevant precision, it will be necessary ‘calculate <strong>for</strong>ward’ from the<br />

data time to the requested time, though the equations necessary are provided in the<br />

GPS and <strong>WAAS</strong> specifications.<br />

Tropospheric corrections will be calculated elsewhere (it is a ‘static’ model and<br />

tropospheric in<strong>for</strong>mation is not transmitted) and can be ignored.<br />

Message Type 12 (<strong>WAAS</strong> network time parameters) are currently not being<br />

broadcast, there<strong>for</strong>e it is assumed that <strong>WAAS</strong> network time = GPS network time.


Initialisation:<br />

Input:<br />

Receiver location in WGS-84 ECEF <strong>for</strong> determining IGPs and <strong>WAAS</strong> satellite (GEO)<br />

suitability.<br />

Function 1: In<strong>for</strong>mation collection and database maintenance.<br />

Input:<br />

<strong>WAAS</strong>/<strong>EGNOS</strong> 250 bit Data packet.<br />

GPS time (millisecond of current GPS week)<br />

Function Description:<br />

In order to process the received <strong>WAAS</strong> in<strong>for</strong>mation and ensure the relevancy of the<br />

received data, an internal <strong>WAAS</strong> database of recently received in<strong>for</strong>mation will have<br />

to be created and maintained. This will be necessary to implement the error<br />

protection protocols inherent in the <strong>WAAS</strong> system.<br />

This function will have to examine the incoming <strong>WAAS</strong>/<strong>EGNOS</strong> messages and<br />

update the internal database.<br />

The CRC of the incoming packet will have to be checked (the packet being rejected<br />

on failure, and some indication of packet failure given), and the Issue of Data<br />

messages contained within the <strong>WAAS</strong> packets analysed in accordance with the<br />

procedure given in the <strong>WAAS</strong> specification (FAA-E-2892B) to ensure the validity of<br />

the data be<strong>for</strong>e entry into the database.<br />

Output:<br />

None<br />

Waas/Egnos Packet<br />

GPS Time<br />

Check Packet CRC<br />

If the packet valid,<br />

and the contained in<strong>for</strong>mation satisfies all of the ‘Issue of<br />

Data’ and ‘Time of Applicability’ conditions, update<br />

internal Waas database.


Function 2: Generation of Satellite Corrections <strong>for</strong> a given SV<br />

Inputs:<br />

GPS time (millisecond of current GPS week)<br />

Satellite (SV) PRN Number<br />

Function Description:<br />

This function will output in<strong>for</strong>mation on a specified satellite, calculated from the<br />

received <strong>WAAS</strong> in<strong>for</strong>mation. Again, received in<strong>for</strong>mation will have to be stored<br />

internally <strong>for</strong> later use, as the transmission of certain message types is irregular.<br />

Each message type, or section of message may have a ‘Time of Applicability’, after<br />

which the in<strong>for</strong>mation should not be used, and these will have to be checked be<strong>for</strong>e<br />

application of the data.<br />

For example:<br />

In order to calculate the ionospheric corrections <strong>for</strong> a specified satellite, firstly the<br />

location of the receiver must be known in order to select store and process the<br />

Ionospheric in<strong>for</strong>mation. The nearest ionospheric grid points (IGP’s) must be<br />

determined, the pierce point of the ionosphere by the satellite signal and the<br />

Ionospheric Correction (IC i ) calculated. (Specified in FAA-E-2892B)<br />

Output:<br />

If corrections not available <strong>for</strong> PRN:<br />

Message indicating ‘Do not use’, ‘Not Monitored’ , ‘Corrections not available’ etc.<br />

If <strong>WAAS</strong>/<strong>EGNOS</strong> corrections available <strong>for</strong> given PRN:<br />

Equivalent to a line of the table below, giving the following calculated to the<br />

requested GPS Time:<br />

Positional corrections with respect toWGS-84 ECEF co-ordinate system <strong>for</strong> the<br />

named satellite, taking into account the long term and fast corrections, as specified in<br />

FAA-E-2892B Sections 4.4.3, 4.4.7, and 4.48.<br />

Clock time error estimate <strong>for</strong> the named satellite.<br />

UDRE (Integrity) of the fast and long term error corrections (combined)<br />

Pseudorange (RMS i ) error estimate <strong>for</strong> the named satellite.<br />

Ionospheric corrections (IC i ), using techniques described in FAA-E-2892B sections<br />

4.4.9 to 4.4.10<br />

Integrity of Ionospheric corrections (σ 2 UIVE)<br />

Residual error (σ 2 flt) as specified in FAA-E-2892B sections 4.5.1 to 4.5.2.


Function2: Calculation of Satellite Corrections.<br />

SV PRN No.<br />

GPS Time in<br />

‘milliseconds of week’<br />

Calculate <strong>WAAS</strong> corrections <strong>for</strong> given SV<br />

PRN, <strong>for</strong> given GPS Time, and output<br />

corrections table:<br />

Position<br />

Corrections<br />

(WGS-84<br />

ECEF)<br />

Clock<br />

Time<br />

Error<br />

Estimate.<br />

Fast<br />

Corr<br />

Integrity<br />

PseudoRange<br />

RMS Error<br />

Estimate<br />

Ionospheric<br />

Corrections<br />

Integrity<br />

Residual<br />

Errors<br />

m s m m m s s 2 m 2<br />

δx δy δz δ∆t SV (t k PRC i UDRE RMS i IC i σ 2 UIVE σ 2 flt


Function 3:<br />

Inputs:<br />

GPS time (millisecond of current GPS week)<br />

GEO (<strong>WAAS</strong>) PRN Number<br />

Function Description:<br />

This function should accept the PRN number of a GEO (Geostationary<br />

<strong>WAAS</strong>/<strong>EGNOS</strong> satellite) and a GPS time, and calculate the position of the specified<br />

satellite at the requested time using all of the GEO satellite in<strong>for</strong>mation previously<br />

decoded and stored from GEO navigation messages.<br />

Output:<br />

GEO satellite position in WGS-84 ECEF coordinate system, using stored GEO<br />

navigation and almanac in<strong>for</strong>mation to calculate position using error corrections to be<br />

correct at the requested time as specified in FAA-E-2892B sections 4.4.11<br />

GEO PRN<br />

No.<br />

GPS Time in<br />

‘milliseconds of week’<br />

Calculate <strong>WAAS</strong> positions <strong>for</strong> given GEO<br />

PRN and GPS Time, and output GEO Position<br />

at requested GPS time.<br />

GEO<br />

PRN<br />

GEO Position<br />

(WGS-84 ECEF)<br />

User<br />

Range<br />

Accuracy<br />

m m m m<br />

PRN X G Y G Z G URA

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