![]() OPERATION MANUAL |
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Clearwater Instrumentation, Inc.
304 Pleasant Street
Watertown, MA 02181
924-2708 Tel (617) 924-2724 Fax
CLEARWATER ARGOS/GPS MARKER BUOY.
OPERATION.
Starting and Stopping Buoy Transmissions.
Altering Buoy Transmission Cycles
SEA SURFACE TEMPERATURE OPTION.
GPS OPTION.
POWER PACK.
ARGOS MESSAGE DATA CONVERSION.
Argos technical file.
Data Conversion for GPS Bytes 1 - 24.
GPS Argos message.
General information: Bytes 1 - 4.
Date Bytes: 5 - 8
Universal Time Bytes: 9 - 12.
Latitude Bytes: 13 - 16.
Longitude Bytes: 17 - 20.
Checksums Bytes: 21-24.
Data Conversion for Temperature (Optional) Bytes: 25-28.
7. BATTERY CARE AND REPLACEMENT.
TABLES |
| Table Duty Cycle Mode Selection |
| Table Battery Life |
| GPS/Argos Technical File |
| Table Argos/GPS Data Format |
The ClearSat Argos/GPS Marker Buoy is a satellite-tracked buoy which facilitates the location of drifting objects anywhere in the world's oceans. When the buoy is activated, an Argos transmitter (PTT) sends a brief radio signal (401.65 MHz), which allows the buoy to be tracked by low earth orbit satellites. The high frequency permits use of a compact, low-profile antenna which fits inside the 30-cm. diameter spherical hull. The entire buoy projects no more than 20 cm above the sea surface. In addition, the Argos message format needs only brief transmissions (320 milliseconds) every 90 seconds to acquire high quality locations and accurate data transmissions.
Transmitted PTT signals from the buoy are received by CLS/Argos uplink receivers on NOAA Tiros satellites when they pass over the buoy. CLS/Argos decodes the signals, computes a buoy location and makes the information available to the user in a variety of forms, including email and phone-accessible database. The computed locations are evaluated statistically and classed according to their calculated accuracy. Location quality, or class, is affected by RF (PTT) signal strength and quality, number of messages received during the satellite pass, altitude of the pass, and sea state. Location classes vary from 1 to 3. Location 3, the most precise class, is accurate to 150 meters (two standard deviations); location 2 to 350 meters; and location 1 to 1 kilometer. Accuracy refers to the statistical distribution of measured locations about the actual location.
NOAA Tiros satellites are in near-polar sun-synchronous orbits at 300 to 400 miles altitude. They complete an orbit around the earth once every 90 minutes. There are usually a minimum of two Tiros satellites receiving Argos PTT signals at any time. A PTT at the equator sees no less than six passes a day. The frequency of satellite passes increases poleward.
Locations of the GPS Marker Buoy are provided by CLS/Argos and by a GPS (Global Positioning System) engine controlled by the marker buoy's microprocessor. Buoy locations are calculated and disseminated by CLS/Argos; Argos locations are accurate to between 300 and 1000 m, depending on the quality of the location. The GPS engine obtains locations which are transmitted by the buoy's radio in an Argos message. GPS locations are generally accurate to less than 100 m. By using transmitted information from CLS/Argos, the user can employ Argos or GPS positioning to follow the buoy. If the user comes within 10 km of the buoy, s/he may use an Argos uplink receiver to obtain transmissions directly from the buoy. Transmissions received in real time include the latest GPS position, which may be used to guide the user to the buoy.
Buoy operation and Argos PTT transmissions are controlled by a magnetic reed switch inside the buoy hull, and metal contacts on top of the hull. A magnet provided with the buoy is attached to a small flat area on the hull, underneath which is the reed switch. The magnet is used to control the reed switch. The magnet used alone starts and stops PTT transmission. The magnet and contacts together are used to set PTT transmission cycles. The figures to the right show the location of the flat area on the base of the sphere with the magnet in place, and without it.
The marker buoy is shipped with a magnet attached as shown above. This prevents the buoy from transmitting before deployment, which would drain the batteries and might incur Argos charges if the PTT signals were picked up by the satellite. After the magnet is removed from the buoy, the transmitter will start PTT transmissions in approximately 90 seconds. PTT transmissions consist of brief bursts spaced approximately 90 seconds apart. Replacing the magnet on the flat area will stop transmissions in approximately 30 seconds. The magnet must be removed for the buoy to transmit. The magnet must be in place to keep the buoy turned off.
Operating in its default mode, Mode 0, the marker buoy will transmit a brief message approximately every 90 seconds, 24 hours a day. CLS/Argos requires intervals between successive transmissions to be varied between 84 and 96 seconds in 1-second steps. Twenty-four hour transmission is called the "continuous" transmission duty cycle. This is the factory default setting.
In addition to continuous transmission, there are four duty cycles with sleep modes of various lengths. The duty cycle can be changed by the user to reduce the number of transmissions by suppressing transmission for intervals of 12, 16, 24, or 48 hours at a time. The period when the marker buoy is not transmitting is called "sleep mode." For instance, when the transmission mode is set to Mode 1, the buoy transmits approximately every 90 seconds for 8 hours, then ceases transmission, or "sleeps," for 16 hours.
Important information about transmission modes is summarized in Table 2.2. ALTERING BUOY TRANSMISSION CYCLES.
| Table 2.2 Duty Cycle Mode Selection. | ||||
Transmission Mode N |
Transmission Cycle, hours |
Magnet "B" On, seconds |
ARGOS Message Byte 0 |
|
|---|---|---|---|---|
| Mode 0, factory default | 24 | > 25 | 000 | |
| Mode 1 | 8 on | 16 off | 5 to 10 | 008 |
| Mode 2 | 12 on | 12 off | 11 to 15 | 012 |
| Mode 3 | 12 on | 24 off | 16 to 20 | 048 |
| Mode 4 | 24 on | 48 off | 21 to 25 | 024 |
When the transmission mode is reset, the new duty cycle of Argos transmission is immediately activated. Transmission mode is not reset when the buoy is turned off for an extended period by replacing the magnet on the hull.
Duty cycles can only be altered by following the steps detailed below. Changing the duty cycle requires a magnet and a length of wire to short (electrically connect) the contacts on the top of the float.
If the marker buoy has the sea surface temperature option, there will be a stainless steel thermistor probe next to the flat area that covers the reed switch. The PTT controller samples the thermistor once a minute and calculates an average sea surface temperature every 15 minutes. Before the end of the first temperature averaging interval, the PTT reports no temperature. Afterwards, temperature averages are updated every 15 minutes and are reported by the PTT in the second and third bytes of the transmitted data string. Conversion of bytes to temperature is discussed below in Section 6, DATA CONVERSION.
The GPS (Global Positioning System) option allows the buoy to acquire and transmit highly accurate positions using the GPS satellite system, which is operated by the U.S. government. GPS positions are obtained approximately every 30 minutes, after which the Argos message is updated to reflect the most recent position. The Argos message reports the year, month, date, UT (Universal Time, accurate to 1 second), and latitude and longitude to +/-0.0001 degree. This close location measurement affords full GPS accuracy (approximately 20 meters) when selective availability is in force. Conversion of the Argos message to date, time and position is discussed below in Section 6, ARGOS MESSAGE DATA CONVERSION.
The Argos Marker Buoy PTT is powered by a 13.5 VDC 56 AH alkaline pack. Marker buoys with GPS are powered by a 12 VDC 112 AH alkaline pack. Each internal parallel unit is diode-protected so that if one of its cells fails, the other packs will not discharge through the failed pack. Table 4.1, Battery Life, shows the available battery power associated with decreasing voltage.
Table Battery Life |
|
| Voltage, VDC | Unused Battery Life, % |
|---|---|
| 12.0 | 100.0 |
| 11.6 | 85.0 |
| 10.7 | 80.0 |
| 9.8 | 70.0 |
| 8.9 | 40.0 |
| 8.0 | 20.0 |
| 7.6 | 15.0 |
| 7.1 | 10.0 |
| 6.7 | 2.0 |
| 6.2 | 0.0 |
The options installed on a marker buoy affect the technical file submitted to Argos, as well as how the Argos message is read. If you have an uplink receiver programmed to decode Argos messages, refer to your manufacturer's manual for how to access the data message from the buoy.
The user should include information in the following Table GPS/Argos Technical File in the Argos application.
Marker buoys equipped with the GPS option report in their Argos message the most recent information obtained from the onboard Argos GPS engine. The data report the year, month, day and UT time, and the latitude and longitude. The information is updated approximately every hour. A general evaluation of the format is presented in Table Argos/GPS Data Format.
A typical Argos data message from the GPS Marker Buoy, with each byte converted to decimal, might look like this:
008 115 001 000 096 001 010 017 018 057 040 025 000 042 036 078 001 071 019 094 019 036 035 027 000 000 147 064
The interpretation of the data is summarized in Table 6.1.
008 115 001 000
Byte 1 = 008, Transmission duty cycle is 8 hour on 16 hours off.
Byte 2 = 115. Battery voltage is 11.5.
Byte 3 = 1. Figure of merit is 1. Figure of Merit is a measure of convergence of
Table GPS/Argos Technical File
ClearSat-2.0 with GPS/Argos Technical File |
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|---|---|---|---|---|---|---|
Sensor No. |
Bits |
Process |
Slope/Intercept |
Min.Mess/Dat |
Max.Mess/Dat |
Datum |
| 1 | 8 | A1 | 0/0 | 48/48 | Duty cycle | |
| 2 | 8 | B1 | 0.1/0.0 | 0/0 | 135/13.5 | Battery, VDC |
| 3 | 8 | A1 | 0/0 | 9/9 | Figure of Merit | |
| 4 | 8 | A1 | 0/0 | 255/255 | Error Message | |
| 5 | 8 | B1 | 1/1900 | 90/1990 | 255/2155 | UT Year |
| 6 | 8 | A1 | 1/1 | 12/12 | UT Month | |
| 7 | 8 | A1 | 1/1 | 31/31 | UT Day | |
| 8 | 8 | A1 | 0/0 | 255/255 | Checksum(2) | |
| 9 | 8 | A1 | 0/0 | 23/23 | UT Hours | |
| 10 | 8 | A1 | 0/0 | 59/59 | UT Minutes | |
| 11 | 8 | A1 | 0/0 | 59/59 | UT Seconds | |
| 12 | 8 | A1 | 0/0 | 255/255 | Checksum(3) | |
| 13 | 8 | A1 | 0/0 | 1/1 | 0 = N; 1 = S | |
| 14 | 8 | A1 | 0/0 | 90/90 | Degrees N/S | |
| 15 | 8 | B1 | 0.01/0 | 0/0 | 99/0.99 | Degrees N/S |
| 16 | 8 | B1 | 0.0001/0 | 0/0 | 99/0.0099 | Degrees N/S |
| 17 | 8 | A1 | 0/0 | 1/1 | 0 = E; 1 = W | |
| 18 | 8 | A1 | 0/0 | 180/180 | Degrees E/W | |
| 19 | 8 | B1 | 0.01/0 | 0/0 | 99/0.99 | Degrees E/W |
| 20 | 8 | B1 | 0.0001/0 | 0/0 | 99/0.0099 | Degrees E/W |
| 21 | 8 | A1 | 0/0 | 255/255 | Checksum(1) | |
| 22 | 8 | A1 | 0/0 | 255/255 | Checksum(4) | |
| 23 | 8 | A1 | 0/0 | 255/255 | Checksum(5) | |
| 24 | 8 | A1 | 0/0 | 255/255 | Checksum(6) | |
| 25 | 8 | A1 | 0.00 | 0.00 | Reserved | |
| 26 | 8 | A1 | 0.00 | 0.00 | Reserved | |
| 27 | 10 | B1 | 0.05/-5.00 | 0/-5.00 | 1023/46.15 | Temperature, C |
Table Argos/GPS Data Format
| Byte 1 Duty Cycle 0, 8, 12, 48, 24 (See Section 2.2) | Byte 2 Battery Voltage13.5 - 7 VDC (See Section 5) | Byte 3 Figure of Merit0 - 9 | Byte 4 Error Message |
| Byte 5 Year90- 256 (add 1900) | Byte 6 Month1 - 12 | Byte 7 Day1 - 31 | Byte 8 Checksum (2): Bytes 5 - 7 |
| Byte 9 Hours0 - 24 | Byte 10 Minutes0 - 59 | Byte 11 Seconds0-59 | Byte 12 Checksum(3): Bytes 8 - 11 |
| Byte 13 LatitudeN = 0, S = 1 | Byte 14 Degrees Latitude0 - 90 | Byte 15 Degrees Latitude, Tenths and Hundredths0.00 - 0.99 | Byte 16 Degrees Latitude: thousandths and ten thousands.0000 - 0.0099 |
| Byte 17 LongitudeE = 0, W = 1 | Byte 18 Degrees Longitude0 - 180 | Byte 19 Degrees Longitude, Tenths and Hundredths0.00 - 0.99 | Byte 20 Degrees Longitude: thousandths and ten thousands.0000 - 0.0099 |
| Byte 21 Checksum(1): Byte 1 - 4 | Byte 22 Checksum Bytes(4): 13 - 16 | Byte 23 Checksum (5):Bytes 17 - 20 | Byte 24 Total Checksum: CKS(1)+CKS(2)+CKS(3)+CKS(4)+CKS(5) |
| Byte 25 (Reserved) | Byte 26 (Reserved) | Byte 27 Temperature, 10 bits including two most significant bits from Byte 26 | Byte 28 Temperature (See Byte 25 and Section 6.1.9) |
navigation solution which is calculated by the GPS engine. Typical results are between 1 and 3:
Byte 4 = 0. There are no error messages.
096 001 010 017
018 036 046 025
6.b.v Latitude Bytes: 13 - 16.
000 042 036 78
001 071 019 092
019 032 033 021
Checksum(1) is evaluated by:
Checksum(4) is evaluated by:
Checksum(5) is evaluated by:
Total Checksum is evaluated by:
Bytes 25 and 26 are reserved and will be zero. Bytes 27 and 28 report temperature, if this option is selected. Ten bits are used to obtain the accuracy (±0.1 °C. Since ARGOS words are eight bits, all eight bits of the third word and the two most significant bits of the fourth word are used to obtain a ten bit number. You can request ARGOS to report the temperature as a decimal and they will perform the conversion, which is described below. Temperature is derived from those words by converting them into a decimal number, or count, which is used in a linear regression equation. Regression coefficients for your drifters are A1 = slope and A1 = intercept.
Here is an example of how to interpret the temperature reading for the data string 000 000 147 064. To obtain temperature "Counts" convert 147 and 064 to binary numbers:
Concatenate the two most significant bits of the second temperature value to the right hand side of the first temperature value and evaluate as a decimal number:
Calculate the temperature from the regression equation where the coefficients are:
You may quickly evaluate the temperature data (this way is just as precise as the explanation given above) as follows:
Using the previous example: