# Presentation: 110471

## Mathematical model of DGPS availability and continuity 

**Mathematical model of DGPS availability and continuity*** *

**Specht C****.**
- Institute of Navigation and Maritime Hydrography
- Naval University in Gdynia
- _[CSpecht@amw.gdynia.pl](mailto:CSpecht@amw.gdynia.pl)_

## contents

- Definitions
- DGPS system structure
- Transmission model
- Comparative analyses of the RTCM messages (types: 1 and 9)
- Software
- Conclusions

## comparable criteria of the navigation systems

**positioning criteria** - characteristics for the system in quality of position fixing. They have in their scope 3 types of accuracy (predictable, repeatable, relative) as well as fix rate, ambiguity and position dimension.
**Reliability criteria** – they form a separate group of indicators with reference to characteristics of exploitation systems. Reliability, _**availability and continuity**_ are among them.
**The safety of exploitation criteria** – their task is to give the user current information about the quality (state) of operating system allowing for the proper level of their utility. So far integrity, the only criterion belonging to this group, has been characterized by a wide range of variables such as: time to alarm, the probability of false alarm etc.** **

## Definitions: Availability

**Working process of system:**

** ****Binary state process of a navigational **
**system operation:**

*Availability [IALA, 1989] is seen as the probability that an aid or system of aids **is **performing a required function under stated conditions at any randomly chosen instant in time. It is shown by the following formula: *

**Availability**** ****of a system can be defined by:**

**Failure moments:**

**Restoration moments:**

**Life times:**

**Failure times:**

**... ****probability that system is in working state at any moment in time.**

**Working process **

## Availability of the navigational system with the exponential distributions of life and failure times:

**Availability of the navigational system with the exponential distributions of life and failure times:**

**Definition: Availability**

*Typical realizations of the operating time of the navigational systems are characterized by the exponential distributions of the lifetime and the time of failures due to the property called the ”memoryless” property**** ***

- - failure rate** **

- - renewal rate** **

- for

- for

- for

- for

*Def: **If  **t** is the life length of a component having exponential life distribution** then*** **

*G(t)* - distribution of the system failure time

*F(t)* - distribution of the system life time** **

- where

- is a function of a renewal stream made of  the renewal moments of the navigational system** **

- For  any distribution...

## Definition: Continuity

**Definition: Continuity**

- For  any distribution...

- At the end of the 90s a new criterion appeared - namely the service continuity.
**Continuity is the probability that the specified system performance will be maintained for the duration of a phase of operation, presuming that the system was available at the beginning of that phase of operation [FRP, 1999]. **
- It seems to be a very essential criterion because the scope of its usage refers to specified period when a navigation object is to use the navigation system to perform a set task provided that at the beginning of it (  t- time) the system was available.
- It should be noted that as it happens in the navigation (maritime or air), the task starts when the system is available.

**For ****exponential distributions of life and failure times**

- - Continuity Time Interval.** **

- - failure rate** **

## DGPS System availability

**The differential GPS** system is the series structure of two subsystems:
**      ****space** – in the aspect of pseudorange measurements ,
**      ****augmentation** (differential GPS transmission) - whose task is to send the differential PRC’s.** **

**Binary state vector of the differential GPS system:**

| - working state of the GPS system, |
| --- |
| - failure state of the GPS system |

| - working state of the AS system, |
| --- |
| - failure state of the AS system. |

- The empirical statistics of the **GPS system availability** are elaborated in detail [SPS 1993; SPS, 2000] so in **further** **considerations we are restricted to analyzing the second of the elements - differential GPS transmission**

**The structure function for the vector  may be written as:**

## Differential GPS transmission methods

- DGPS reference station (code-navigation) can use two types of RTCM messages.
- 	**Message type 1** - all corrections are transmitted in the same frame.
- 	**Message type 9** - number of frames depends on number of corrected GPS satellites.

- Message type 9, due to the format, requires considering three separate cases, depending on the number of satellites situated over the minimal elevation of the DGPS reference station.
- Almost 90 % of time (for 24 SV’s) DGPS reference stations transmit the pseudorange corrections using three RTCM messages type 9.** **

## Availability of Differential GPS transmission

**The differential GPS dates are transmitted in the form of binary sequences. **
**However, the particular bits create higher structures – RTCM messages, in which a failure of even one component (bit) causes neglecting the data of the whole message. **
**Then, while considering the higher structure such as the RTCM message, it can be noticed that though the DGPS receiver decodes correctly a single RTCM message (i.e. 9-3) containing corrections to only 3 satellites, this will not prevent solving the navigational problem in the sense of determining the coordinates of position (latitude, longitude, height). **

- We conclude that the differential GPS transmission system is available under the following conditions (conjunction of events):
**The user receiver received a sufficient number of pseudorange corrections for position determination. **
**The age of pseudorange corrections is lower than the arbitrarily accepted.**

## Availability of Differential GPS transmission

_**Availability of Differential GPS transmission**_

**The availability will be the state in which the age of at least 4 pseudorange corrections related to various satellites is lower than the maximum****.**** **

## The process of PRCs transmission for Ns ={7,8,9} 

***Age of corrections (often) doesn’t constant multiple of message length (in seconds).***
***	***
***	******for R=100 bps and message 9-3 time of transmission takes 2.1 sec.***
***	******when SA was on recommended age of correction was 30 sec.***
***It cause that two delta periods (odd and even) occurs with ***_***different availability.***_

## Availability of DGPS transmission

_**t**__**he process of PRCs transmission for N**__**s**__** ={7,8,9}**__** **_

**The binary state vectors (which characterised the structure of message transmission) for two deltas**** :**

**and  the functions of their structures (when structure is in working state (availability): **

## Availability of DGPS transmission

**After decompositi****on (process from binary value ****- ****states to probability)****:**

**AVAILABILITY:**

_**Availability of DGPS transmission**_
_**t**__**he process of PRCs transmission for N**__**s**__** ={7,8,9}**__** **_

## Transmission availability software (step 1)

**DGPS RS**** signal strength level**

**Dedicated software for coverage calculations:**
- The shoreline combined of 100 000 points was vectorized,
- database of ground conductivity and dielectric constant was added,
- Millington’s method  was used to calculate the field strength of beacons’ signal (groundwave).
- Signal strength level [in dBu] is calculated base on single point signal measurement or on the  ERP of the beacon.

**Common area**

**Vectori****z****ed map**

**Port of Gdynia**

## Transmission availability software (step 2)

**Noise level**** NTIA reports (3D)**

**=****SNR=f(BER)**

*RAPORT 85-173 of The National Telecommunications and International Administration**** ***

**DGPS RS**** signal strength level - 3D**

**The input value for mathematical calculation (model) is BER (bit error ratio)****,**
**BER could be calculated based on the relation between signal strength level and noise level****,**
**Atmospheric noise level is calculated based on NTIA reports,**
**Signal strength ****level ****is calculated based on Millington method.**

**Signal strength level**

**Noise**** level**

## Transmission availability software (step 3)

**DGPS t****ransmission availability**** zones**

_**Transmission availability **__**software**__** (**__**step 3**__**)**_

**SNR=f(BER)**

**Transmission model**

**Software INPUTS:**
**Signal strength level at single point **
**Message: RTCM 1 and 9.**
**Baund rate: 100 or 200 bps.**
**Age of corrections: variable.**

## some comparative analyses ...

**The increase in the number of satellites, for which the reference station transmits pseudorange corrections by message RTCM type 9-3, improves the availability **

**Type of the message, bound rate vs BER**

**Availability of RTCM 1 as a sat number function**

**higher transmission rate – higher availability,**
**message type 1 has lower availability than type 9-3,**
**coverage for RTCM no 9-3 could be wider than for type 1**
** ****(the same availability can be archives with the lower SNR).**

**h****igher number of satellites causes lower availability****,**
**o****ptimal value is ****7****-10 satellites****.**

**RTCM 1**

**RTCM 9-3**

## Continuity of Differential GPS transmission

_**Continuity **__**of **__**Differential GPS transmission**_

**DGPS transmission continuity**** zones**** – Polish DGPS RS Rozewie**

**Software INPUTS:**
**Message: RTCM 1 and 9.**
**Baund rate: 100 or 200 bps.**
**Age of corrections: variable.**
**Continuity time interval: variable.**

**Availability refers to ****single moment in time****,**
**Continuity refers to ****time period where the availability of the system in the starting point is 1****.**
**Reliability refers to ****time period**** (availability of the system in the starting point could be differ than 1).**
**The continuity is calculated based on availability model presuming that system was available in the starting point and ****different failures are independent**** (memoryless process**** – exponential distribution****)****. **

## Conclusions

**The problem was important because of the lack of methods, which would enable the parameter prognosis with regard to the process of navigation. **
**In this light, the problem reliability characteristics constitutes one of the fundamental issues for multi-criteria assessment of modern systems at the stage of system testing and exploitation as well. **
**The theory worked out has been referred to the probabilistic characteristics of navigation systems functioning such as expected value, variance, or standard deviation of lifetimes and times of failures. **
**The specialised sof****t****ware was made for availability and continuity prediction. **

_**Conclusions**_