/
Assistant Professor in the TELECOM Group Assistant Professor in the TELECOM Group

Assistant Professor in the TELECOM Group - PowerPoint Presentation

syfarect
syfarect . @syfarect
Follow
342 views
Uploaded On 2020-06-16

Assistant Professor in the TELECOM Group - PPT Presentation

Carl Milner ENAC ENAC 8 th March 2018 RAMS for GNSS Questions 2 How to relate the Tolerable Hazard Rate per hour to the positioning function per epochsampletest Correlation time impacts Fault Free case and Faulty case ID: 779332

sis time gnss rams time sis rams gnss wp1 2018 webex brainstorming system availability unavailable risk repair pnt level

Share:

Link:

Embed:

Download Presentation from below link

Download The PPT/PDF document "Assistant Professor in the TELECOM Group" is the property of its rightful owner. Permission is granted to download and print the materials on this web site for personal, non-commercial use only, and to display it on your personal computer provided you do not modify the materials and that you retain all copyright notices contained in the materials. By downloading content from our website, you accept the terms of this agreement.


Presentation Transcript

Slide1

Assistant Professor in the TELECOM Group

Carl

Milner

– ENAC

ENAC |8

th

March 2018

RAMS for GNSS

Slide2

Questions

2

How to relate the Tolerable Hazard Rate per hour to the positioning function per epoch/sample/test?Correlation time impacts (Fault Free case and Faulty case)

What conditions may be defined around the use of GNSS in rail? Is there a known probabilistic distribution for them?

 average riskIs there reasonable means to predict?  specific riskHow to measure/ensure maintainability for GNSS applications?WP1 Brainstorming

Webex, 12/02/2018

Slide3

RAMS vs GNSS SIS

3

Positioning, Navigation and Timing (PNT)

In aviation, the active Navigation System provides the primary guidance function. Navigation System Error (NSE) is then the difference between the true position and estimated position.

Signal-In-Space (SIS) performance requirements express the quality of a GNSS PNT service assuming a fault-free receiver, meaning one which is operating nominallySIS performance includes nominal errors which are local to the aircraft, namely multipath and receiver noise which have been modelled and validated by Boeing (Wozniak, 1997) and Airbus “3.7.2.4.1 The combination of GNSS elements and a fault-free GNSS user receiver shall meet the signal-in-space requirements defined in Table 3.7.2.4-1” (ICAO SARPS, 2010)

WP1 Brainstorming

Webex, 12/02/2018

Slide4

RAMS vs GNSS SIS

4

WP1 Brainstorming

Webex

, 12/02/2018Safety RiskSafety Risk from Aircraft Failure

SIS Safety Risk

RX

Navigation System

Safety Risk

Slide5

RAMS vs GNSS SIS

5

WP1 Brainstorming

Webex

, 12/02/2018Safety RiskSafety Risk from Aircraft Failure

SIS Safety Risk

RX

Navigation System

Safety Risk

Slide6

RAMS vs GNSS SIS

6

SIS Requirements - Accuracy

(Absolute) Accuracy The degree of conformance between the estimated position and the true position of the aircraft at a given time (95% 2𝜎)

Most conservative/likely definitionPredictable Accuracy: The accuracy of a PNT systems position solution with respect to the charted solution Close to absolute Accuracy (could be used in rail)Repeatable Accuracy: The accuracy which a user can return to a location whose coordinate has been measured at a previous time Not to be usedRelative Accuracy: The accuracy with which a user can measure position relative to that of another user at the same time Unlikely but possible application in moving block (or more appropriately under virtual coupling)

WP1 Brainstorming

Webex, 12/02/2018

Slide7

RAMS vs GNSS SIS

7

SIS / PNT RequirementsIntegrity

The measure of trust that can be placed in the information provided by the PNT system, including the ability to provide timely warnings when the system should not be usedTime-to-Alert Allowable time from the onset of an unsafe condition to the alarm indication

Integrity Risk The allowable probability of an undetected unsafe conditionSpecific Risk The probability of unsafe conditions subject to the assumption that all credible unknown events that could be known occur with a probability of one “The approach integrity requirements apply in any one landing and require fail- safe design. If the specific risk on a given approach is known to exceed this requirement, the operation should not be conducted” (DeCleene 2005)Average Risk The probability of unsafe conditions based upon the convolved estimated probabilities of all unknown eventsWP1 Brainstorming

Webex, 12/02/2018

e.g

.

for 1 operation

 

e.g

. <

over many operations

 

Slide8

RAMS vs GNSS SIS

8

SIS / PNT RequirementsContinuity

Continuity of a system is the ability of the system to perform its function without interruption during the intended operation i.e. the probability that the specified performance will be maintained for the duration of a phase of operation “The continuity requirement should be applied as applying the average risk of loss of service”

Availability The percentage of time that the services of a system are available (accuracy and integrity are met, in some interpretations also continuity)Reliability The probability that a system will perform its function within defined performance limits for a specified period of time (not the operation duration)WP1 BrainstormingWebex, 12/02/2018

Slide9

RAMS vs GNSS SIS

9

WP1 Brainstorming

Webex

, 12/02/2018

Slide10

RAMS vs GNSS SIS

10

RAMS

Reliability The probability that a system can perform a required function under given conditions for a given time interval

for an interval if failure rate is constant

MTTF Mean Time To Failure (MTTF) which for a constant rate is equal to

Maintainability The probability that a given active maintenance action, for an item under given conditions of use can be carried out within a stated time interval when maintenance is performed under stated conditions and using stated procedures

Mean

Time To

Repair

Availability

The

ability

of a

product

to

be

in a state to

perform

a

required

function

under

given

conditions at a

given

instant of time or over a

given

time

interval

(if constant rates)

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide11

RAMS vs GNSS SIS

11

RAMS

Safety Freedom from unacceptable

risk of harmRisk The probable rate of occurance of a hazard causing harm and the degree

of severity of harm

Safety

Integrity

Likelihood of a system satisfactorily performing the required safety functions

under all the stated conditions

within a stated period of time

Dependability Collective term used to describe the availability performance and its

influencing factors

Quality of Service

Eg

Percentage of trains arriving with delay less than X minutes as a result of the PNT function

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide12

RAMS vs GNSS SIS

12

WP1 Brainstorming

Webex

, 12/02/2018

Slide13

RAMS vs GNSS SIS

13

What influences dependability/quality of service…?

ReliabilityMaintainabilityTime duration of operations

High High Many trains with small-medium delayLow Low

Few trains with long delays and cancellationsSimilar

availability Averaging instantaneous availability gives availability but loses information regarding reliability

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide14

RAMS vs GNSS SIS

14

System States

Available + Safe

‘Failed’/Unavailable/Outage

Available + Unsafe

Failure

Rate

 

Repair

Rate

 

<THR

WP1 Brainstorming

Webex

, 12/02/2018

?

Slide15

RAMS vs GNSS SIS

15

First Mapping

WP1 Brainstorming

Webex, 12/02/2018

Slide16

RAMS vs GNSS SIS

16

RAMS Safety Integrity vs PNT Integrity

SIL expressed by Tolerable Hazard RateHazard Rate may be averaged over the time interval? i.e.

Over 1 hour? Over all time? Over the Time-To-Alert period? Or must be met for any interval however small?Requirements at the algorithmic level are needed for each epochAviation integrity, the high-level requirement is for within the defined period of operatione.g. for SBAS when converted to a single epoch a number of independent samples is used

(operational level)

Correlation time of 360s (ionosphere driven)

(receiver level)

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide17

RAMS vs GNSS SIS

17

Alert Limit – no agreement:2.5m for track discrimination/station operations

20-25m for along-track positioningor might also be expressed as a function of speed

Time-to-alert – values between 1s and 5sWP1 BrainstormingWebex, 12/02/2018

Slide18

RAMS vs GNSS SIS

18

What would be the response of the rail network to a ‘Predictable’ outage?

Continuity in aviation is a safety issue vs. Reliability in RAMS is notReliability and Availability are directly linked in RAMS

The PNT service is available in civil aviation even if an aircraft experiences a loss of continuity (standard interpretation)Predictable outages are not continuity risks (not universal agreement on interpretation, depends upon system developmentNavigation systems may be sole/primary/supplemental meansMitigations for loss of serviceSince global availability and probability of a down state switch depend upon many factors (including the solution proposed), the requirement used for detection thresholds (continuity) should be set lateWP1 Brainstorming

Webex, 12/02/2018

Slide19

RAMS vs GNSS SIS

19

Loss of Reliability (Failures)Immobilising

ServiceMinor

WP1 BrainstormingWebex, 12/02/2018

Slide20

RAMS vs GNSS SIS

20

WP1 Brainstorming

Webex

, 12/02/2018

Slide21

RAMS vs GNSS SIS

21

Loss of Availability/ContinuityPredictable

Slow geometry change  increased protection level (or real time integrity risk) 

unavailable  time  repairSatellite loss passing horizon  increased protection level  unavailable  time  repairSatellite loss due to planned manoeuvre/maintenance (NANU warning)  increased protection level  unavailable  time  control 

repairMasking  loss of tracking  geometry change  increased protection level  unavailable  location  user 

repair

UnpredictableFalse alarm 

failed exclusion  unavailable

 time  repair

Satellite failure  correct detection

 failed exclusion

 unavailable  time  control 

repair

Ionosphere gradient

c

orrect detection

failed exclusion

unavailable

 time 

repair

Extreme multipath

c

orrect detection

failed exclusion

unavailable

 time 

repair

Interference

loss of tracking

geometry change

 increased protection level 

unavailable

 time 

repair

Jamming

loss of tracking

geometry change

 increased protection level 

unavailable

 time  security 

repair

Scintillation  loss of tracking  geometry change  increased protection level 

unavailable

 time 

repair

Shadowing  loss of tracking  geometry change  increased protection level 

unavailable

 time  user 

repair

Change in error models (i.e. from DGNSS)  increased protection level 

unavailable

 time  user 

repair

WP1 Brainstorming

Webex

, 12/02/2018

Slide22

RAMS vs GNSS SIS

22

Instantaneous Availability (Up-State vs. Down-State)

where:

is the true train location

and

is the time (and constellation phasing state)

is the set of satellites (all sets are numerated by

up to

)

is the availability function given the geometry defined by

and other parameters which may modify the requirement such as speed

where:

is the state probability of satellite set

being available for positioning as a result of phenomena indexed by

depending upon the assessment methodology (probabilistic simulation of the environment?)

may be influenced by deterministic changes of

(e.g. predictable masking)

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide23

WP1 RAMS vs SIS/PNT

23

The

are for most not under the control of the (rail PNT system) designer

In the case of false alarm/correct detection and failed exclusion events, the probabilities are. However, under this formulation, the thresholds are set in order to meet availability targetsGiven values for each sub-condition event probabilities (i.e. probability of ionosphere gradient

etc) the availability function is well-defined

To assess through simulation

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide24

WP1 RAMS vs SIS/PNT

24

(Operational/Signal Environment) Reliability and Maintainability would then be products

of the Availability function and not the reverse.For example, given either a route for an operation:

Where:

is the repair rate from

to

for outage reason

Also may be assessed through simulation either over an ‘average’ 1 hour period and track or more locally

Must loop over constellation

 

 

 

 

 

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide25

WP1 RAMS vs SIS/PNT

25

Reliability (defined this way) may learn from aviation’s

Continuity however.Continuity allocated amongst cases by considering impact upon number of aircraft i.e.

With an allocation of

and a maximum of 100 aircraft impacted then if

the user receiver

requirement would be

rather than

if only a single aircraft be impacted

Domino effect for a rail GNSS outage under moving block – should reliability account for this?

Does reliability already consider differently failures which impact the multiple vehicles and those that

Impact just a single one?

 

WP1 Brainstorming

Webex

, 12/02/2018

Slide26

This project has received funding from the European Union’s Horizon 2020 research and innovation

programme

under Grant Agreement No 777561

Call identifier: H2020-S2RJU-2017

Topic: S2R-OC-IP2-01-2017 – Operational conditions of the

signalling

and automation systems;

signalling

system hazard analysis and GNSS SIS characterization along with Formal Method application in railway field