J3,30DK,00,3.5 Navman Wireless, J3,30DK,00,3.5 Datasheet - Page 8

DEV KIT FOR JUPITER 3 AND J3-30

J3,30DK,00,3.5

Manufacturer Part Number
J3,30DK,00,3.5
Description
DEV KIT FOR JUPITER 3 AND J3-30
Manufacturer
Navman Wireless
Type
Receiver, GPSr
Datasheet

Specifications of J3,30DK,00,3.5

Frequency
1575.42MHz
For Use With/related Products
Jupiter 3, J3-30
Lead Free Status / RoHS Status
Lead free / RoHS Compliant
Other names
943-1006
Jupiter 3-30
3.7 Sensitivity
Sensitivity of the Jupiter 3-30 is measured assuming a system noise value of 3 dB. The sensitivity values are as follows:
3.8 Dynamic constraints
The Jupiter 3-30 receiver is programmed to deliberately lose track if any of the following limits is exceeded:
3.9 Position and velocity accuracy
The position and velocity accuracy of the Jupiter 30 are shown in Table 3-3, assuming full accuracy C/A code. These values are
the same in normal operation and when Adaptive TricklePower is active.
4.0 Multi-mode aiding
Multi-mode aiding technology makes navigation information available to GPS devices when enough Satellite Vehicles (SVs) are
not visible due to obstruction. In autonomous operation mode, the GPS receiver requires a signal level of 28 dBHz or higher in
four or more SVs to download ephemerides. This requires an uninterrupted full 30 seconds of data reception from each SV. If
the data isn’t received in full, the ephemeris data collection has to start again at the next cycle.
The type of multi-mode aiding currently supported by the Jupiter 3-30 is Ephemeris Push. This feature supports live ephemeris
data to be downloaded from application servers that allows hot start performance at all times including in weak conditions and
moving start ups. The ephemeris would typically be valid for 4 hours until the live ephemeris is downloaded or new ephemeris
data is provided.
To use with this Ephemeris Push, the live ephemeris data is collected at application servers and then transmitted to the GPS
receiver through a network connection. An application note about Ephemeris Push is in preparation and will be available at a
later date.
velocity: 500 m/s max
acceleration: 4 G (39.2 m/s2) max
vehiclejerk: 5 m/s3 max
altitude: 18 000 m max (referenced to MSL)
Navman Wireless OEM Solutions • 27171 Burbank -Suite 200; Foothill Ranch, CA 92610-2501
TEL: +(949) 461-7150 • FAX: +(949) 461-7860 • www.navmanwirelessoem.com
|
 Parameter
acquisition – cold start
acquisition – hot start
navigation
tracking
Datasheet
 Parameter
horizontal CEP*
horizontal (2 dRMS)
vertical VEP*
velocity (speed)**
velocity (heading)**
** I n 3D Kalman filtered mode in steady state open sky conditions
* position error 50% and under normal open sky conditions
Table 3-3: Position and velocity accuracy
Table 3-2: Sensitivity
SignalStrength
–145 dBm
–155 dBm
–158 dBm
–159 dBm
< 0.01m/s
< 0.01°
Value
2.5 m
5.5 m
2.0 m
25 dBHz
15 dBHz
12 dBHz
10 dBHz
C/n
0

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