There seems to be no technical data about this rx all over the internet. So I took the papers I got with my rx and here you can see the result. Here are details of the used data format.
Sometimes I'm in doubt about the English they used, but I wrote it down 'as it is'.
Simultaneously, by receiving up to 8 satellites parallelly and by making position to employ information of all received satellites (all-in-view positioning technology), it is possible to attain high accuray positioning.
Even if three satellites which are normaly necessary for positioning are not received, with two satellite reception, it is possible to make positioning where short time blockage of satellites.
With intake of GPS satellite correction data which is generated at the reference station, it is possible to make high accuracy postioning drastically.
It is 40% down-sized than the previous model. to save associate materials for integration and improve reliability, it can be installed on the Customer's board, which does not require pin connector and connection cable. With direct antenna connection to the receiver unit, inner antenna coaxial cable together with connector is not required anymore.
By containing the receiver board in the aluminium box, it minimizes its electro-magnetic generation.
| Receiving method | 8 channels |
| Receiving frequency | 1575.42 MHz (L1), C/A code |
| Sensitivity | -130 dBm (Antenna input level of antenna system as described) |
| Dynamic range | More than 25 dB |
| Accuracy | |
|
100m 2DRMS (HDOP<3, SA on, without Direct DGPS, final GPS system accuracy |
|
0.9 m/s RMS |
| Dynamic capability | |
|
680 km/h |
|
2 g |
| Position calculation interval | normally 1 s |
| Fixing calculation | use all satellites tracked |
| Time to first fix (no signal loss) | |
| a) Hot TTFF | 21 to 56s with initial position, time, date, almanac and ephemeris data. Condition of maximum TTFF is twice detection failure of satellite signal. |
| b) Warm TTFF | 33 to 130s with initial position, time, date, almanac data (no ephemeris data). Condition of maximum TTFF is twice detection failure of satellite signal. |
| c) Cold TTFF | 95s to 11min with no data |
| Re-acquisition time | Average 8s after signal obstruction of less than 10s |
| Modes of operation | Automatic selection of 2D/3D |
| Data Interface TX1, RX1 | TTL direct connection, 4800Bd |
| Data Interface RX2 | TTL direct connection, 4800Bd (?) |
| Input data for direct DGPS (RX2 port) | Specified by RTCM SC104 Version 2.0 Note: only Type I and Type II data are used for correction calculation (1200Bd, no parity, 1 stop bit) |
| Age of differential DGPS data limit | If correction ceases for receiving, the values in use will continued to be treated as valid for a further 30s |
| RF connector | SMB (same as UM type made by HIROSE) |
| Power requirement | |
| a) Main (operating) | DC +5V +/- 0.25V, ripple within 10mVp-p 210mA typ., 1.05W typ. (w/o antenna) |
| b) Back up (standby) | DC +2.2 to 3.6V (no Li battery on GPS board), 60µA maximum |
| Available power for antenna preamp. | DC +4 to 5V, 10mA to 30mA |
| Antenna Failure | |
| a) Short detection | more than 30mA |
| b) Open detection | less than 10mA |
| 41.0mm x 86.0mm x 24.5mm (w/o connector) |
| Temperature | |
| Operating temperature | -10°C to +60°C |
| Storage temperature | -30°C to 85°C |
An antenna with a preamplifier is available from a variety of our selections. However, if the customer provides, the following are the specifications in case that the loss of coaxial cable between praamplifier and RF input of CCA-191P is less than 7dB.
Antenna with preamplifier
| Frequency | 1575.42+/-1MHz |
| Gain (antenna) | > -5dBi (0 to 85 deg.) |
| Gain (preamplifier) | 32dB +/- 3dB |
| Noise figure (preamplifier) | 1.5dB max. |
| Power supply | DC +3.9V or more at 30mA DC +5.1V or below at 10mA |
| Output VSWR | 1.5 max. |
| Output impedance | 50 Ohms |