1 / 38

ARGOS LOCATION CALCULATION - PowerPoint PPT Presentation

Roland Liaubet (CLS) liaubet@cls.fr Jean-Pierre Malardé (CLS) malarde@cls.fr. ARGOS LOCATION CALCULATION. Argos location principles Standard location processing description Others types of location Argos location class definition, interpretation and limits

I am the owner, or an agent authorized to act on behalf of the owner, of the copyrighted work described.

ARGOS LOCATION CALCULATION

An Image/Link below is provided (as is) to download presentation

Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author.While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server.

- - - - - - - - - - - - - - - - - - - - - - - - - - E N D - - - - - - - - - - - - - - - - - - - - - - - - - -

Presentation Transcript

Roland Liaubet (CLS)

liaubet@cls.fr

Jean-Pierre Malardé (CLS)

malarde@cls.fr

ARGOS LOCATIONCALCULATION

Argos location principles

Standard location processing description

Others types of location

Argos location class definition, interpretation and limits

Argos location : main causes of error

How to improve your number of locations and their accuracy

Argos location software improvements foreseen

Summary

Location based on Doppler shift measured on each message

Argos location principles

Apparent frequency shift observed

when the receiver and the transmitter

are in motion relative to each other

TCA Time of Closest Approach

CTA Cross Track Angle

Doppler curve characteristicsTCA/CTA definition

Distance too short

Doppler shift

Sub-satellite track

Cross

Track

Angle

CTA

TX

Time of closest

approach

TCA

Time

Distance

too long

CTA also called distance from the ground sat track

3 Hypothesis :

Transmission frequency is stable during the satellite pass

The platform is motionless during the satellite pass ( in principle)

the altitude is known

Argos location principles

The location process follows 7 steps:

A priori checks

Geometric initialization

Newton linearization

Least-squares method

Removing ambiguity

Plausibility checks

Location class estimation

Standard location processing

Standard location is attempted if at least 4 messages are received during a satellite pass

3 parameters are calculated :

latitude,

longitude,

transmission frequency

Standard location processing

1 : A priori checks

TX frequency calculated from the previous satellite pass

2 messages -> 2 Doppler shifts -> 2 cones

Intersection with ellipsoid = 2 positions

Which is the true position?

Which is the mirror position?

Standard location processing

2 - Geometric initialization

V1

V2

Standard location processing

4 : Least-squares method

Minimize the quantity :

IC = SQRT (|| AX-F||2) = SQRT [ Σni=1( Fri – Fci)2/ (n-3)]

The iterative processing

stops when the residual

error does not change

significantly from an

iteration to the next one

Fr

IC = internal consistency or residual error

Convergence

towards the

true position

Convergence

towards the

mirror position

Standard location processing

5 : Removing ambiguity

Satellite

ground

track

Where :

K : is the coefficient corresponding to the probability that the actual location of the transmitter is inside the circle with radius R. K = 1,414…corresponds to a probability of approximately 63% (*)

HDOP : is the horizontal dilution of precision (*)

Q: is the frequency noise estimator ( residual error)

B: is the orbit error (B=100 m)

The radius R of the circle of error is given by:

(*) Argos location is assumed to be a bi-normal distribution

(*) HDOP can be interpreted as the geometrical factor of observation error propagation

Good HDOP

T=120s

T=60s

T=30s

HDOP effect on location accuracy

At 8°, error = 1.414*200*0.25 ~ 70 m

At 2°, error = 1.414*600*0.25 ~212 m

TX at the horizon

(2500km)

TX closed

to sat track

Effect of the PTT position relative to satellite ground track

Curves

intersection

is not precise

Poor HDOP

Curves

intersection

is not precise

Poor HDOP

Curves

intersection

is optimal

Good HDOP

Residual error translates random errors

Modeling errors or bias errors ( except for orbit error) are not taken into account in the ARGOS location and underestimated when calculating the radius of the circle of error

Classification limits

Only latitude and longitude are calculated. We assume the transmission frequency has not changed since the last location ( CLASS B)

A priori checks

Geometric initialization

Removing ambiguity

1 criterion :minimum distance traveled from last location

Plausibility checks

2 criteria:

Solution selected matches minimum distance traveled from the previous location

Distance traveled from the previous location is compatible with the maximum velocity of the platform

Two-message location processing

Location accuracy depends chiefly on the difference between the transmission frequency used in the geometric initialization and the actual PTT transmission frequency

Two-message location

Latitude, longitude and transmission frequency are calculated. We assume the transmission frequency noise is negligible ( CLASS A)

A priori checks

Geometric initialization

Newton linearization

Resolution of a precisely determined linear system

Removing ambiguity

Frequency continuity with respect to the last calculated frequency

Minimum distance traveled from last location

Plausibility checks

Transmitter frequency of the chosen solution is significantly closer to the previous calculated frequency than than the one of the solution candidate

Minimum distance traveled from last location

Distance traveled from the previous location is compatible with the maximum velocity of the platform

Three message location

The platform is assumed to be moving from its previous location with a mean velocity in latitude and longitude ( and during the current satellite pass)

Standard location assuming a moving PTT

Standard locations only

0.5 h < delta T < 3.5 h

Pnew

Plast

The new location is kept if the residual error (IC) is smaller than the one obtained for a stationary platform

Argos location : main sources of error

- timestamp

- orbit error

Hardware

- ionosphere

- troposphere

TX power

- relativistic effect

Hardware

- Speed

- Altitude

- CTA

Error caused by frequency drift( due to temperature variation )

Doppler shift without freq. drift

Measured Doppler shift

Real position

Computed position

Drift

errors : USO quality

Error due to platform speed

Error due to frequency drift

400 m

7 km

Elat(m) = 200*Vlat(km/h)

Elon(m) = 100*Vlon(km/h)

Error of altitude

Error due topropagation in ionosphere

2.0 km

0.5 km

Impact of output power

PTT 18781 - CLASSES 1,2,3 - KL

Nesdis data streams

100

90

2W

80

70

60

%

50

40

0,25 W

30

20

10

0

0

250

500

750

1000

1250

1500

1750

2000

Distance from the true position (m)

How to improve your locations

• How to increase the number of messages received per satellite pass

• How to improve the location accuracy

Number of locations :Today, not enough messages received per satellite pass : it is the biggest cause of location problems

Several explanations can be put forward :

repetition rate too low,

hardware quality and antenna efficiency,

TX signal power too weak,

TX environment (surrounding noise),

data loss due to system occupancy ( TX concentration and transmission at the same frequency).

More location & better Precision

How to increase the number of messages received and improve location accuracy

Use multi-satellite service,

Select good quality USO ( CLASS A recommended)

Tuning TX parameters such as :

output power,

repetition rate,

transmission frequency ( outside the Argos 1 band)

Declare platform (average) altitude

Declare correct maximum velocity of the platform

More locations & better Precision

Current status

PTT altitude is assumed to be known

An error in PTT altitude is translated into an error varying between ½ and 4 times on longitude

Command MOD is not much used

Land platforms represent 20 %

DEM : digital Elevation Model

USGS Model

30’’ arc resolution / 100 m accuracy (  1000 m)

Statistic in the European zone

Altitude declared at the User Office : 0 m in 93 % of cases

Altitude error greater than 100 m in 40%

Experimentation

Dh = 1000m

Dh = 0m

Using a DEM

Multi-pass location

• Current status :

• Only single pass location

• Seven satellites in operation

• Waiting time between two successive satellite overpasses at 43 ° latitude :

• 5 % : less than 5 minutes

• 25 % : less than 10 minutes

• 57 % : less than 15 minutes

Selected

PTT Location

Example

Multi-pass location