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LA000507G © 2006 Navman New Zealand. All rights reserved. Proprietary information and specifications subject to change without notice.

3.2 Acquisition times

Table 3‑1 shows the corresponding TTFF times for each of the acquisition modes.

Mode

J20

J20S

J20D

Typ

90%

Typ

90%

Typ

90%

TTFF hot  

(valid almanac, position, time & ephemeris)

8 s

12 s

8 s

12 s

8 s

12 s

TTFF warm  

(valid almanac, position & time)

38 s

42 s

38 s

40 s

35 s

40 s

TTFF cold  

(valid almanac)

44 s

55 s

45 s

56 s

52 s

70 s

re‑acquisition 

 

(<10 s obstruction with valid almanac, 

position, time & ephemeris)

100 ms 100 ms 100 ms 100 ms 100 ms 100 ms

Table 3-1: TTFF acquisition times

3.3 Timing 1PPS output

The 1PPS (Pulse Per Second) output of the Jupiter 20 receiver is < 1 µs, typical ± 300 ns in 

reference to UTC (Coordinated Universal Time). This feature is currently only available on the 

Jupiter 20 standard module.

3.4 Battery backup 

(SRAM/RTC backup)

During powered down conditions, the SRAM and RTC may be kept operating by supplying 

power from the VBATT as shown in Table 4‑1. The Jupiter 20 can accept slow VBATT supply 

rise time (unlike many other SiRFstar

II

 based receivers) due to an on‑board voltage detector.

3.5 TricklePower mode

During normal mode of operation the Jupiter 20 is continuously running, providing a navigation 

solution at the maximum rate of once per second. This continuous mode provides no power 

saving.

The TricklePower mode of operation can be enabled to reduce the average power consumption. 

The main power is supplied to the module continuously. An internal timer wakes the processor 

from sleep mode. The module computes a navigation position fix, after which the processor 

reverts to sleep mode. The duty cycle is controlled by a user‑configurable parameter.
If ephemeris data becomes outdated, the TricklePower mode will attempt to refresh the data set 

within every 30‑minute period, or for every new satellite that comes into view.
With TricklePower set to a 20% duty cycle, a power saving of 50% can easily be achieved with 

minimal degradation in navigation performance.

3.5.1 Adaptive TricklePower

 

mode

In Adaptive TricklePower mode, the processor automatically returns to full power when signal 

levels are below the level at which they can be tracked in TricklePower mode. This is the 

default behaviour when TricklePower is active.

3.5.2 Push-To-Fix mode

Unlike TricklePower, the operation in this mode is not cyclic. This mode always forces the 

GPS software to revert to a continuous sleep mode after a navigation position fix. It will stay 

in sleep mode until woken by activation of the reset input, and compute a fresh position.
If the ephemeris data becomes invalid, the RTC has the ability to self activate and refresh the 

data, thus keeping the restart TTFF very short.
This mode yields the lowest power consumption of the module, and is ideal where a battery 

powered application requires very few position fixes.

For further information on the TricklePower and Push‑To‑Fix modes refer to the Low Power 

Operating Modes application note (LA000513).

Содержание LA000508

Страница 1: ...0 GPS receiver module Data Sheet Related documents Jupiter 20 Integrator s manual LA000508 Jupiter 20 Product brief LA000509 Jupiter Series development kit guide LA000645 SiRF Binary protocol referenc...

Страница 2: ...ng 1PPS output 7 3 4 Battery backup SRAM RTC backup 7 3 5 TricklePower mode 7 3 5 1 Adaptive TricklePower mode 7 3 5 2 Push To Fix mode 7 3 6 Differential aiding 8 3 6 1 Differential GPS DGPS 8 3 6 2...

Страница 3: ...compliance 16 9 6 Disposal 16 10 0 Ordering information 17 11 0 Glossary and acronyms 17 Figures Figure 2 1 Jupiter 20 module architecture 4 Figure 8 1 Jupiter 20 mechanical layout 15 Tables Table 3...

Страница 4: ...ironments The interface configuration allows incorporation into many existing devices and legacy designs The Jupiter 20 receiver decodes and processes signals from all visible GPS satellites These sat...

Страница 5: ...oved if the battery backup is connected Reset generator There are two voltage threshold reset generators in the Jupiter 20 The first provides a reset to the baseband block if the main power drops belo...

Страница 6: ...ype character 8 product revision characters 9 13 sequential serial number 3 0 Performance characteristics 3 1 TTFF Time To First Fix TTFF is the actual time required by a GPS receiver to achieve a pos...

Страница 7: ...reduce the average power consumption The main power is supplied to the module continuously An internal timer wakes the processor from sleep mode The module computes a navigation position fix after whi...

Страница 8: ...e available or when a fixed altitude value can be used to produce an acceptable navigation solution the receiver will enter 2D navigation mode using a fixed value of altitude determined by the host Fo...

Страница 9: ...t a velocity greater than 5 km h Table 3 4 Position and velocity accuracy 4 0 Electrical requirements 4 1 Power supply 4 1 1 Primary power The Jupiter 20 GPS receiver is designed to operate from a sin...

Страница 10: ...is antenna should be in the range of 20dB to 30dB 4 1 7 Burnout protection The receiver accepts without risk of damage a signal of 10dBm from 0 to 2GHz carrier frequency except in band 1560 to 1590 MH...

Страница 11: ...SPI bus VIH min 2 0V VIH max PWR_IN 0 1V VIL min 0 1V VIL max 0 8V VOH min at IOH 2mA 2 0V VOH max PWR_IN VOL min 0 VOL max at IOL 2mA 1 0V Reset input max capacitance Cmax 100pF input current max 600...

Страница 12: ...igh 10 GND P ground 11 GND P ground 12 GND P ground 13 GND P ground 14 GND P ground 15 GND P ground 16 GND P ground 17 RF_IN I antenna signal input 18 GND P ground 19 V_ANT P external power supply for...

Страница 13: ...ach NMEA message is contained in the Navman NMEA reference manual MN000315 NMEA message J20 J20S J20D GGA 1s 1s 1s GSA 1s 1s 1s GSV 1s 1s 1s RMC 1s 1s 1s VTG 1s 1s 1s GLL 1s 1s 1s ZDA 1s N A N A PTTK...

Страница 14: ...Acquires satellites and continues tracking in extremely low signal environments yes Low signal navigation Continues navigating in extremely low signal environments yes 1 PPS A timing signal generated...

Страница 15: ...The Jupiter 20 Development kit series assists in the integration of the Jupiter 20 module in custom applications The Development kit contains all of the necessary hardware and software to carry out a...

Страница 16: ...C standard J STD 033 Handling Packing Shipping and Use of Moisture Reflow Sensitive Surface Mount Devices 9 3 ESD sensitivity The Jupiter 20 GPS receiver contains class 1 devices and is ESDS ElectroSt...

Страница 17: ...receivers within the same general geographic area GDOP Geometric Dilution of Precision A factor used to describe the effect of the satellite geometry on the position and time accuracy of the GPS recei...

Страница 18: ...S WITHOUT WARRANTY OF ANY KIND EITHER EXPRESSED OR IMPLIED RELATING TO SALE AND OR USE OF NAVMAN PRODUCTS INCLUDING LIABILITY OR WARRANTIES RELATING TO FITNESS FOR A PARTICULAR PURPOSE CONSEQUENTIAL O...

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