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COSPAS-SARSAT (International Satellite System for Search and Rescue Services)

Overview    User Segment   Spacecraft   Payloads (LEO)   Mission Status     Ground Segment   Payloads (GEO)   References

The COSPAS-SARSAT system is an international, humanitarian satellite-based search and rescue system and service which can detect and locate transmissions from emergency beacons carried by ships, aircraft, or people -- which operates 24 hours a day, 365 days a year. Use of the COSPAS-SARSAT system is free to the beacon operator. Once the rescue signals are detected and verified (located) by the system, search and rescue operations can be initiated.

COSPAS (Cosmicheskaya Systyema Poiska Aariynyich Sudov) which translates to (Space System for the Search of Distressed Vessels), and SARSAT (Search & Rescue Satellite Aided Tracking System) payloads are part of an international cooperative satellite-based radiolocation system to support search and rescue operations for aviators, mariners, and land travellers in distress. COSPAS is the original system developed by Russia (former Soviet Union) in the mid-1970s; SARSAT was developed in parallel by France, Canada, and the USA. 1) 2)

The COSPAS-SARSAT system provides distress alert and location data to RCCs (Rescue Coordination Centers) for 121.5 MHz beacons within the coverage area of COSPAS-SARSAT ground stations, referred to as LUTs (Local User Terminals), and for 406 MHz beacons activated anywhere in the world. The overall system concept is illustrated in Figure 3. The nominal system configuration comprises two COSPAS and two SARSAT payloads on polar-orbiting satellites. Russia provides two COSPAS satellites in near-polar orbits at an average altitude of 1000 km (83º inclination). The USA supplies two NOAA POES satellites with on-board SARSAT payloads provided by Canada and France. The orbital period for each satellites is about 100 minutes, the footprint of the COSPAS-SARSAT visibility is in the order of 4000 km in diameter. The first COSPAS payload was launched on June 29, 1982, while the first SARSAT equipment was flown on NOAA-8, launched in March 1983. Note: The Nadezhda ("Hope") spacecraft series are modified "Tsikada" satellites of Russia that are being used in support of navigation services and/or of COSPAS-SARSAT services (the launch site is Plesetsk, Russia). 3) 4) 5)

Note: The interested reader is referred to the homepage of COSPAS-SARSAT (reference 1) for detailed documentation on all aspects of the system. This file can only serve for a quick overview of the system.

 

Background:

The early SAR history started in the 1960s when light aircraft and some marine vessels started carrying small, battery-operated radio transmitters, operating at the international distress frequency of 121.5 MHz, that could be activated in an emergency distress situation. Such transmitters, called Emergency Locator Transmitters (ELTs) on aircraft, and Emergency Position Indicating Radio Beacons (EPIRBs) on ships, emitted a low-power signal that could be picked up by a receiver in a nearby air traffic control tower or by an aircraft in the vicinity, thus providing only line-of-sight coverage if one was searching in that location. - By the mid-1970s, more than 250,000 distress beacons were in service in Canada, Europe and the USA. Lives of aviators and mariners were being saved thanks to these transmitters, but there was still room for improvement, particularly as it was now the `space age'. 6) 7) 8) 9) 10) 11)

• The beginnings of SARSAT date back to 1970 when a plane carrying two U.S. congressmen crashed in a remote region of Alaska. A massive search and rescue effort was mounted, but to this day, no trace of them or their aircraft has ever been found. In reaction to this tragedy, the US congress mandated that all aircraft in the United States carry an Emergency Locator Transmitter (ELT). This device was designed to automatically activate after a crash and transmit a homing signal.

• On May 6, 1977 the USSR and USA signed the COSPAS-SARSAT Treaty covering deployment of an international system of emergency beacon receivers aboard satellites.

• On November 23, 1979 a Memorandum of Agreement was signed by the agencies of USA, Russia (i.e., the former USSR), Canada, and France on the implementation of the COSPAS-SARSAT system. Under this Memorandum of Agreement, Russia built and launched LEO satellites with the COSPAS payload [on Tsikada and Nadezhda (Hope) satellite series], while the USA carried the SAR payloads, built by Canada and France, on their NOAA weather satellites (POES series) for the SARSAT system. Note: the Memorandum of Agreement is also referred to as ICSPA (International COSPAS-SARSAT Program Agreement).

• The first LEO satellite in the COSPAS-SARSAT system was launched on June 29, 1982 by the former USSR (see Table 3). The COSPAS-SARSAT system was declared operational in 1985. 12)

• The first GEO satellite in the COSPAS-SARSAT system with a GEOSAR (Geostationary Search and Rescue) payload was flown on the NOAA satellite GOES‐7 (launch Feb. 26, 1987).

• In 1988 the four space segment providers signed an agreement which ensures service continuity and availability of the system to all States on a non-discriminatory basis - this is referred to as the "International COSPAS-SARSAT Program Agreement." The International COSPAS-SARSAT Program Agreement established a Council and a Secretariat. The Council oversees the implementation of the Agreement and coordinates the activities of the Parties. The Secretariat, the permanent administrative organ of the Program, takes directions from the Council. The international COSPAS-SARSAT Secretariat is located in London, UK (at Inmarsat).

• ISRO introduced the COSPAS‐SARSAT service over the Indian Ocean in 1992 with its SASAR (Satellite Aided Search and Rescue) payload flown on the GEO INSAT-2 series, starting with INSAT-2A (launch July 9, 1992). GEOSAR is also flown on the MSG series of EUMETSAT (launch of MSG‐1 Aug. 28, 2002, renamed to Meteosat‐8 as of Jan. 29, 2004 when the operational service officially started). 13)

In 2004, the participating countries and organizations of the COSPAS-SARSAT program included:

- The four parties to the COSPAS-SARSAT International Program Agreement [Canada (CRC), France (CNES), Russia (ROSHYDROMET), and the USA (NOAA)] that provide and operate the satellites and the ground segment equipment

- 24 ground segment providers that operate ground receiving stations the Local User Terminals (LUTs) and Mission Control Centers (MCCs) for the worldwide distribution of distress alerts (over 40 LUTs for LEOSAR - also referred to as LEOLUTs)

- Nine participants associated with the management of the system.

Note: Several countries participating in COSPAS-SARSAT service are represented by their SAR agency or a maritime or aviation agency, rather than their space agency.

• In 2005, Montreal, Canada became the new home of the Cospas-Sarsat Program office.

• In early 2007, ISRO (Indian Space Research Organization) signed a formal Understanding with COSPAS-SARSAT concerning the long-term provision of INSAT GEOSAR services.

On February 1, 2009 an era of emergency beacon support ended: the 121.5 and 243 MHz emergency beacons were phased out for satellite distress alerting (in accordance with the 2000 Council decision). The decision to stop satellite processing of 121.5 / 243 MHz signals is due to problems in this frequency band which inundate search and rescue authorities with poor accuracy and numerous false alerts, adversely impacting the effectiveness of lifesaving services. 14) 15)

Thirty years after the inception of COSPAS-SARSAT, a new chapter is opening for the international program: analog beacons have been phased out, digital 406 Mhz beacons are fully operational, new generation SARSAT-3 instruments are launch on the US NOAA satellites and the European MetOp satellites. Furthermore, the COSPAS-SARSAT organization is preparing the future, with the integration of a MEOSAR component that will use the GNSS (Global Navigation Satellite Systems) constellations.

 


 

Alert Signal Devices (User Segment)

There are three types of radiobeacon devices (heritage of older rescue services) in use, namely maritime EPIRBs, aviation ELTs, and personal locator beacons (PLBs). 16) 17)

1) EPIRB (Emergency Position Indicating Radio Beacon) for use in maritime applications. A small battery-powered transmitting device which is carried on vessels (several nations require EPIRB devices on all vessels). It can be activated in times of trouble to send out help signals. EPIRB devices operate on a frequency of 121.5/243 MHz (the 243 MHz frequency is used only in some older beacons), they may also include the 406.025 MHz alert signal for global detection.

Introduction of new EPIRB technology in 2009: The 406 MHz EPIRB emits a low power, 25 mW sweeping-tone signal constantly on 121.5 MHz, but emits a 5 W burst about every 52 seconds at 406 MHz. Hence, the 406 MHz emission is 200 times stronger than the 25 mW sweeping-tone signal. If the EPIRB is equipped with an internal or external GPS capability, not only can the 406 MHz DF (Direction Finder) accurately track the course to the 406 MHz signal, but future capabilities will allow the operator to read a GPS position on a monitor inside the search aircraft. Proper registration of a beacon can further assist SAR services by providing immediate access to data critical to mission success.

2) ELT (Emergency Locator Transmitter) for aviation use. The 121.5 MHz band service emergency beacons are required on many aircraft, referred to as ELT 121.5, with a smaller number carried on maritime vessels. The 121.5 MHz frequency band is used by an older type of beacons which do not transmit any encoded information. It is also the frequency used for low-power homing transmitters included in most beacons. The more recent ELT devices on aircraft are provided with dual frequency alert systems, 121.5 and 406.025 MHz.

The development of the new generation of beacons transmitting at 406 MHz commenced at the beginning of the COSPAS-SARSAT project in the mid-1970s. Although the COSPAS-SARSAT system was primarily designed to function on the much improved 406 MHz frequency, it still had to make a provision for the thousands of 121.5 MHz beacons already in use. For this reason, the satellites were designed to receive 121.5 MHz as well.

The 406 MHz units were designed specifically for satellite detection and Doppler location by having:

- High peak power output and a low duty cycle

- Improved radio frequency stability

- A unique identification code in each beacon

- Digital transmissions that could be stored in a satellite's memory

- A spectrum dedicated by the ITU (International Telecommunication Union) solely for distress beacons.

The 406 MHz beacons transmit a 5 W, half-second burst approximately every 50 seconds. The carrier frequency is phase-modulated with a digital message. The low duty cycle provides a multiple-access capability of more than 90 beacons operating simultaneously in view of a polar orbiting LEO satellite, versus only about 10 for 121.5 MHz beacons.

3) PLB (Personal Locator Beacon) used for land-based applications (basically an ELT when carried by a person, but not used in aviation or maritime applications). These are handheld or pocket size dual frequency (121.5 and 406 MHz) or single frequency (either 121.5 or 406.025 MHz) devices which transmit distress signals to search and rescue authorities via the COSPAS-SARSAT satellite system. On July 1, 2003, FCC (Federal Communication Commission) of the USA authorized the use of PLBs (406 MHz digitally encoded) on a nationwide basis.

At the start of the 21st century, there are more than 30 manufacturers of 406 MHz beacons in 12 countries, and many more distributors around the world, with over 100 different models type-approved by COSPAS-SARSAT. The number of 406 MHz beacons in use has increased dramatically from zero in 1985 to 20,000 in 1990 and to about 350,000 today.

The international Council of COSPAS-SARSAT decided in October 2000 [in response to guidance from the IMO (International Maritime Organization) and the ICAO (International Civil Aviation)] to cease processing the 121.5 MHz analog signals by satellite on 1 February 2009. From that date on, only the 406 MHz beacons will be detected by satellite. The decision was made to reduce the chronically high false alarm rate from analog distress beacons. Currently 97 percent of analog distress beacon signals are false alarms.

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Figure 1: Illustration of typical PLBs (Personal Locator Beacon) systems (image credit: NOAA)

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Figure 2: Overall system configuration of COSPAS-SARSAT (image credit: COSPAS-SARSAT)

 


 

Space segment of COSPAS-SARSAT:

The overall COSPAS-SARSAT system architecture (space segment) includes two types of satellites to collect and relay emergency messages from the ground segment: 18) 19)

• Spacecraft in LEO (Low Earth Orbit) carrying either the COSPAS or the SARSAT payload (generically referred to as LEOSAR). The LEOSAR system is the longest one in use.

• Spacecraft in GEO (Geostationary Earth Orbit) carrying an SAR payload (generically referred to as GEOSAR).

• Spacecraft in MEO (Medium Earth Orbit) carrying the MEOSAR (MEOSAR)payload. This service refers to plans to install a MEOSAR secondary payload on the navigation satellite constellations (GPS, GLONASS, and Galileo) - starting in about 2013.

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Figure 3: System elements of Search and Rescue Satellites

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Figure 4: The initial participants in COSPAS-SARSAT: Nadezhda, POES & GOES of NOAA (clockwise from lower right), image credit: CNES

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Figure 5: Schematic of the COSPAS-SARSAT space segment (image credit: COSPAS-SARSAT) new version as of Feb. 1, 2009

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Figure 6: Schematic of the COSPAS-SARSAT space segment (image credit: COSPAS-SARSAT) old version

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Figure 7: Illustration of COSPAS-SARSAT spacecraft in LEO (image credit: COSPAS-SARSAT)

 


 

Satellite Payloads (LEO Space Segment or LEOSAR)

The nominal LEO satellite constellation consists of four spacecraft payloads, two SARSAT and two COSPAS providing parallel services for 121.5 MHz and 406 MHz beacons.

This system worked well, and is still in use today (2008). However, the LEOSAR configuration has inherent time delays, ranging from minutes to hours, in detecting and relaying distress signals because the low altitude satellites (< 1000 km) view only a small portion of the Earth at any instant as they circle the globe. In particular, the LEO system could not be made much better for 121.5 MHz beacons, due to technical limitations of the beacons and the radio channel.

The original LEO system also carried payloads that allowed for the implementation of new digital distress beacons operating at 406 MHz, far superior to the original analog 121.5 MHz beacons. Beacons with the 406.025 MHz signal transmit digitally encoded information which may include beacon identification (which allow COSPAS-SARSAT services to access registration data bases providing additional information on the unit in distress), and beacon location data (determined by satellite navigation devices such as flown on GPS or GLONASS spacecraft). The new beacons at 406.025 MHz permit the distress location to be automatically computed by the satellite system ten times more accurately (to within 2 km) and the beacon user to be identified, whereas the old 1960s technology beacons at 121.5 MHz gave only an approximate location (to within 20 km) and no user identification, since the 'wow, wow, wow' sound of the signal was similar for all these beacons.

In addition, the 406 MHz system provides global coverage for beacons activated anywhere on Earth, as the beacon signals are stored onboard the satellite and retransmitted to each ground station as the satellite orbits the Earth.

SARSAT (Search and Rescue Satellite Payload)

The SARSAT payload consists of SARR (SARSAT Repeater), provided by CRC/Canada [National Search and Rescue Secretariat (NSS) is funding SARR while DND (Department of National Defense)]; SARP (SARSAT Processor), provided by CNES/France, and the antenna system provided by the USA. The SAR service problem requires two basic functions for effective SAR operations to take place, namely: 1) alerting and 2) locating. The alerting function only requires a low-capacity one-way communications system. The locating function, however, places far more demands on the system. The overall system uses low-powered battery-operated distress transmitters that are received by polar orbiting satellites with an SAR subsystem on-board.

The SAR concept exploits the Doppler shift resulting from relative motion between the distress transmitter and the polar orbiting satellite. A successful alert requires at least one satellite pass over the distress area to detect a signal and locate the position of the emergency transmitter. In some cases a second pass may be required to resolve ambiguity. 20)

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Figure 8: SARSAT instrument package valid up to SARSAT-10 (NOAA-18, launch May 20, 2005), image credit: NOAA

The SARSAT payload consist of a 2-band (121.5 MHz and 406.05 MHz) repeater SARR and a 406.025 MHz processor SARP. The SARR downlink is at 1544.5 MHz and, besides the two repeated bands, also includes the 2400 bit/s bit stream SARP output. The 121.5 and 406 MHz bands are also serviced by two Russian COSPAS satellites which, together with the NOAA satellites, provide timeliness of response. 21)

Spacecraft Repeater (121.5, 243, and 406 MHz)

Bandwidths (Doppler shift + drift + Tolerance + guardband)

Parameter

Specification

121.5 MHz

25 kHz (bandwidth)

243 MHz

46 kHz

406.050 MHz

100 kHz

Transmitter power (1,544 MHz)

8 W decibels referenced to a watt (dBW)

Physical Characteristics

Mass, size, power

24 kg, 0.034 m3, 53 W

Spacecraft 406 MHz Processor

Max bandwidth, storage capacity, output data rate

80 kHz, 324 kbit, 2.4 kbit/s

Physical characteristics

Mass, size, power

27.5 kg, 0.034 m3, 33 W

Table 1: SARSAT subsystem parameters

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Figure 9: Illustration of the SARR instrument (image credit: NOAA)

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Figure 10: Illustration of the SARP subsystems (image credit: NASA)

Each SARP (SARP) is composed of a receiver processor, referred to as DRU (Data Recovery Unit), FF (Frame Formatter), and a memory unit. Each SARP is configured redundantly. Throughout the service history of COSPAS-SARSAT there existed various implementations/configurations of SARP, namely:

• SARP-1 (Search And Rescue Processor-1): The SARP-1 package was installed on all early spacecraft in the COSPAS as well as in the SARSAT series.

• SARP-2 (Search And Rescue Processor-2): The SARP-2 package has improved performance in system capacity, bandwidth, and protection against interferers. Both long and short messages are supported by this processor. The first SARP-2 configurations were implemented on the NOAA-15 spacecraft (launch May 13, 1998) with the SARSAT-7 payload, as well as on the Nadezhda-7 spacecraft of Russia (launch Sept. 26, 2002) with the COSPAS-10 payload.

• SARP-3 (Search And Rescue Processor-3): SARP-3 is an improved onboard device which was introduced for the first time on the MetOp-A spacecraft of EUMETSAT (launch October 19, 2006). SARP-3 receives and processes emergency signals from the 406 MHz beacons on aircraft and ships in distress. It determines the name, frequency and time of the signal. These preprocessed data are then fed in real-time to the SARR (Search And Rescue Repeater) instrument for immediate transmission to the SARSAT (Search and Rescue Satellite) distress terminals in the ground segment (referred to as LUTs).22) 23)

The objective of SARP-3 is to detect and locate ELTs (Emergency Locator Transmitters), EPIRBs (Emergency Position-Indicating Radio Beacons), and PLBs (Personal Locator Beacons) operating at 406.05 MHz. SARP-3 detects the signal from 406.05 MHz beacons and stores the information for subsequent downlink to a LUT (Local User Terminal). Thus, global detection of 406.05 MHz emergency beacons is provided which is a requirement of the GMDSS (Global Maritime Distress Safety System). After receipt of information from a satellite's SARP, a LUT locates the beacons by Doppler processing. The principle of the Doppler processing is that a transmitter signal will have different frequencies depending on its location in relation to the receiver. The determined beacon frequency by the SARP-3 differs depending on the relative velocity between beacon transmitter and the SARP-3 receiver. The 406.05 MHz beacons are located with an accuracy of ~ 4 km. The LUT forwards the located distress message to a nearby Mission Control Center (MCC), which forwards the information to a Rescue Coordination Center (RCC).

Note: SARP systems of SARSAT-11 or higher (Table 3) are using the SARP-3 instrument package.

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Figure 11: Functional block diagram of the SARSAT SARP-3 (image credit: COSPAS-SARSAT)


COSPAS (Space System for Search of Vessels in Distress)

The USSR (Union of Soviet Socialist Republics) began deploying the space segment with the launch of Cosmos 1383 on June 30, 1982 from Plesetsk into a 989 km x 1028 km, 83º inclination orbit (Tsikada is a first generation navigational satellite series). Designated as COSPAS-1, the 121.5 MHz band remained operational until December 1987, with 406 MHz utilized primarily for interference monitoring. Cosmos 1447 (launched March 24, 1983) and 1574 (June 21, 1984) adopted the roles of COSPAS 2 and 3, with a third vehicle available as replacement. The COSPAS payload normally shares the Nadezda (Hope) satellite platform with a Doppler navigation payload of the Tsikada system.

The COSPAS payload is composed of the following elements: a SARR (SARSAT Repeater), a SARP (SARSAT Processor), and uplink and downlink antennas. The SARR provides local mode coverage for the 121.5 MHz band and its parameters. The SARP provides both local mode and global mode coverage for the 406 MHz band. COSPAS payloads may have one of two possible SARP configurations installed: SARP with memory (SARP-1) or an improved SARP with memory (SARP-2). The SARP-2 instrument has improved performance in system capacity, bandwidth, and protection against interferers. Both long and short messages are supported by this processor (Ref.23).

The COSPAS repeater (Figure 15), SARR, is redundantly configured and consists of the following units: a) two dual-conversion receivers; b) two 4.0 W phase modulated L-band transmitters; and c) two Power, Telemetry and Command (PTC) units.

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Figure 12: Functional block diagram of the COSPAS system (image credit: COSPAS-SARSAT)

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Figure 13: Functional block diagram of the SARSAT-TIROS (POES) payload and S/C with SARR-1 or SARR-2 and SARP-2 or SARP-3 (image credit: COSPAS-SARSAT)

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Figure 14: Functional block diagram of the SARSAT-MetOp and SARSAT-NPOESS payload and S/C with SARR-1 or SARR-2 and SARP-2 or SARP-3 (image credit: COSPAS-SARSAT)

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Figure 15: Functional block diagram of the COSPAS Repeater (image credit: COSPAS-SARSAT)

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Figure 16: Functional block diagram of SARSAT SARR-1 repeater (SARSAT-13 and earlier), image credit: COSPAS-SARSAT)

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Figure 17: Functional block diagram of SARSAT SARR-2 repeater (SARSAT-14 and after), image credit: COSPAS-SARSAT)

 


 

COSPAS-SARSAT system status:

LEOSAR and GEOSAR Systems: As of June 2015, the APSAR/TF/4 report noted that five LEOSAR spacecraft were in operation: Sarsat-7, Sarsat-10, Sarsat-11, Sarsat-12 and Sarsat-13. Planned LEOSAR launches include the Russian Cospas-13 and Cospas-14 in 2016 and 2017, respectively, and the U.S. LEOSAR program in the process of planning and funding of a dedicated LEO satellite to be launched into an ascending early afternoon orbit, no earlier than 2019. 24)

- Seven satellites operating at full operational capability (FOC) comprise the GEOSAR space segment as at 26 June 2015: two Indian geostationary satellites, INSAT-3A at 93.5º E (presently not fully in service) and INSAT-3D at 82º E; two U.S. geostationary satellites, GOES-15 (West) at 135º W and GOES-13 (East) at 75º W; two EUMETSAT geostationary satellites, MSG-2 (9.5° E) and MSG-3 (0°); and one Russian geostationary satellite Electro-L1 operated at 76º E. Russia's Louch-5A remains under test at position 167ºE, with New Zealand, the United States and Australia supporting Russia in evaluating the Louch GEOSAR performance, with an aim of commissioning the satellite into the GEOSAR constellation. The GEOSAR constellation will be further maintained with the anticipated launch of Electro-L2 (2015), MSG-4 (2015), and GOES-R, -S, -T, and -U (2016, 2017, 2019 and 2025, respectively).

- As at 26 June 2015, 53 LEOLUTs, 23 GEOLUTs and 31 MCCs were in operation.

• June 2015, MEOSAR update: The MEOSAR satellites orbit the Earth at altitudes ranging from 19,000 to 24,000 km. The primary missions for the satellites used in the three MEOSAR constellations are their respective Global Navigation Satellite Systems (GPS, Galileo and GLONASS).25)

- All MEOSAR satellite constellations use transparent repeater instruments to relay 406 MHz beacon signals, without on board processing, data storage, or demodulation. The SAR/Galileo and SAR/GLONASS payloads operate with downlinks in the 1544 – 1545 MHz band (L- band) and the GPS-DASS uses the S-band at 2226 MHz (experimental).

- As of 1 June 2015, the status of MEOSAR payloads is: GPS/DASS – 17, SAR/Galileo – 6, SAR-GLONASS – 2.

MEOSAR Constellation

GPS-DASS (S-band)

GLONASS K

GALILEO (IOV+FOC)

SAR-GPS (L-band)

Number of active satellites

17/24

2/24

6/24

0/24

Number of orbital planes

6

3

3

6

Orbital inclination

55º

64º

56º

55º

Orbital altitude

20,180 km

19,140 km

23,222 km

20,180 km

Orbital period

11 h 58 m

11 h 15 m

14 h 22 m

11 h 58 m

Uplink polarization

LHCP

RHCP

RHCP

LHCP

Downlink frequency/polarization

2226 MHz RHCP

1544.9 MHz LHCP

1544.1 MHz LHCP

1544.9 MHz RHCP

Status

Experimental payloads (S-band)*

In Test

Operational

In Development

First launch date

January 2001

February 2011

October 2012

Planned 2020

Table 2: Key parameters of all the constellations available on 1 June 2015

*Note: GPS/DASS satellites are S-band satellites. They are viewed as experimental payloads and cannot therefore be considered for long-term MEOSAR operations. Their operational use on a temporary basis for the MEOSAR EOC and IOC (Initial Operating Capability) is authorized, however.

• LEOSAR and GEOSAR Systems: As of 1 December 2014, five LEOSAR spacecraft were in operation: SARSAT-7, SARSAT-10, SARSAT-11, SARSAT-12 and SARSAT-13. SARSAT-8 was decommissioned on 8 June 2014 after a spacecraft bus failure. Planned LEOSAR launches include the Russian Cospas-13 and Cospas-14 in 2016 and 2017 respectively, and the U.S. LEOSAR program in the process of planning and funding of a dedicated LEO satellite to be launched into an ascending early afternoon orbit, no earlier than 2019. 26)

- Seven satellites operating at FOC (Full Operational Capability) comprise the GEOSAR space segment as of 1 December 2014: two Indian geostationary satellites, INSAT-3A at 93.5º E and INSAT-3D at 82º E; two U.S. geostationary satellites, GOES-15 (West) at 135º W and GOES-13 (East) at 75º W; two EUMETSAT geostationary satellites, MSG-2 (9.5° E) and MSG-3 (0°); and one Russian geostationary satellite Electro-L1 operated at 76º E. Russia's Louch-5A (also spelled as Luch-5A) remains under test at position 167ºE, with New Zealand, the United States and Australia supporting Russia in evaluating the Louch GEOSAR performance, with an aim of commissioning the satellite into the GEOSAR constellation. On 28 April 2014 Russia launched another Louch-series geostationary satellite (Louch-5V), which remains under IOV (In-Orbit Validation) test. The GEOSAR constellation will be further maintained with the anticipated launch of MSG-4 (2015), GOES-R (2016) and GOES-S (2017).

- MEOSAR Systems: As of December 2014, the MEOSAR satellite constellation currently includes three operational L-band satellites (Glonass-K1, and Galileo IOV-3 and IOV-4 satellites) and 16 GPS II satellites carrying experimental DASS(Distress Alerting Satellite System) repeaters with an S-band downlink used by the Cospas-Sarsat Program. The 16th DASS payload was launched aboard the GPS IIF-8 satellite on October 29, 2014.
The first two Galileo FOC satellites (carrying L-band SAR payloads) were launched on August 22, 2014; however, a launch anomaly occurred and the operational capability of these satellites remains uncertain. It is reported that early in December one of these satellites was successfully moved into a higher orbit with sufficient fuel to operate for 12 years. A similar orbital maneuver was planned for the second one by late December. The Galileo Program intents to complete the in-orbit testing of the first two FOC satellites before launching additional ones. Between six and eight additional FOC satellites are expected to be launched in 2015.
The USA plans to carry Canada-supplied L-band SAR repeaters on 24 GPS satellites beginning with the launch of the ninth GPS Block III satellite, anticipated for deployment as early as 2020.

• In 2013, Cospas-Sarsat alert data assisted in 720 distress incidents (634 in 2012) and 2,156 persons were rescued (2,029 in 2012). Since September 1982, the Cospas-Sarsat System has provided assistance in rescuing at least 37,211 persons in 10,385 SAR events. For aviation, Cospas-Sarsat assisted in 153 incidents, involving the rescue of 348 persons. Cospas-Sarsat provided the only alert in 23 aviation incidents, and the first alert in 65 incidents (Ref. 26).

- Based on information received from manufacturers on beacon production and a standard assumption made about beacons removed from the market at the end of an assumed ten-year service life, there were approximately 1,600,000 406-MHz beacons in use worldwide at the end of 2013, up 6.7% from 2012. The rate of beacon population growth in 2013 was lower than in 2012 (7.5%). The production of beacons capable of acquiring position data from radionavigation satellites (such as GPS and Glonass) and encoding this position information into the transmitted alert data ("location protocol beacons") increased marginally from 61.4% in 2012 to 67.7% in 2013.

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Figure 18: Number of SAR Events and Persons Rescued with the Assistance of Cospas-Sarsat Alert Data (January 1994 to December 2013)

• January 23, 2013: The first switch-on of a Galileo search and rescue package (i.e. MEOSAR) shows it to be working well. Its activation begins a major expansion of the space-based Cospas–Sarsat network, which brings help to air and sea vessels in distress. 27)

- The second pair of Europe's Galileo navigation satellites (IOV-3 and IOV-4) — launched together on October 12, 2012 — are the first of the constellation to host SAR search and rescue repeaters. These can pick up UHF signals from emergency beacons aboard ships and aircraft or carried by individuals, then pass them on to local authorities for rescue.

• In 2010, Cospas-Sarsat will continue work to define the desired operational characteristics of a new generation of 406 MHz beacons at the Experts' Working Group on Next Generation Beacon Requirements, to be held in Washington, D.C., USA in September 2010 (Ref.11).

The next generation satellite system for Cospas-Sarsat, MEOSAR (Medium-altitude Earth Orbiting satellites for Search And Rescue), continues to progress at the technical level. Early operational data availability is planned from 2014, subject to the availability of operational MEOSAR satellites and ground receiving stations (MEOLUTs). The use of MEOSAR satellites will potentially allow evolution of the 406 MHz beacon, which will be both attractive to beacon owners and challenging to system operators. A return link capability, if widely adopted by users, could significantly impact the management of SAR operations. Its introduction will require in depth evaluation and close cooperation with the System's customers, i.e. SAR authorities.

Success can clearly be seen in the ever increasing 406 MHz beacon population, which is forecast to reach one million beacons by the end of 2010.

• The year 2009 marked the 30th anniversary of the signing of the first Cospas-Sarsat Memorandum of Understanding (MOU). This event was celebrated in October 2009 in Montreal, Canada, during 43rd Session of the Cospas-Sarsat Council.

• On February 1, 2009, satellite processing of signals from 121.5 / 243 MHz beacons was terminated. The reason: the 406 MHz beacons have proven superior performance capabilities. They transmit a much stronger signal and are more accurate, verifiable and traceable. 406 MHz distress signals can be accurately detected within a matter of minutes. Each 406 MHz beacon has a unique identifier encoded within its signal. 28)

As of February 2009, the COSPAS-SARSAT system is comprised of: (Ref. 28) 29) 30)

• 5 LEOSAR satellites in LEO (Low Earth Orbit), from 700 to 1,000 km

• 5 GEOSAR satellites

• 45 LUTs receiving signals transmitted by LEOSAR satellites (LEOLUTs)

• 19 LUTs receiving signals transmitted by GEOSAR satellites (GEOLUTs)

• 29 Mission Control Centers for distributing distress alerts to SAR services

• More than 600,000 406 MHz beacons (Figure 19).

• Since the beginning of its operation in September 1982 through the end of 2006, COSPAS-SARSAT provided alerts that assisted in the rescue of more than 22,400 persons in about 6,200 SAR events.

• The participating countries and organizations in COSPAS-SARSAT are: Algeria, Argentina, Australia, Brazil, Canada, Chile, China, Cyprus, Denmark, France, Germany,Greece, Hong Kong, India, Indonesia, Italy, ITDC (International Telecommunication Development Corporation), Japan, Korea, Madagascar, Netherlands, New Zealand, Nigeria, Norway, Pakistan, Peru, Poland, Russia, Saudi Arabia, Singapore, South Africa, Spain, Sweden, Switzerland, Thailand, Tunisia, Turkey, UK, USA, Vietnam.

Cospas_AutoC

Figure 19: Estimated 406 MHz beacon population at the end of 2007 (image credit: COSPAS SARSAT Secretariat)

LEO Satellites in polar or near-polar orbits

Payload

Spacecraft

Launch Date

Status/Comment

Orbit (km)

COSPAS-1

Cosmos 1383

June 29, 1982

Decommissioned (March 1988)

989 x1082, 83º

COSPAS-2

Cosmos 1447

Mar. 24, 1983

Decommissioned (Dec. 1989)

959 x 1013, 83º

COSPAS-3

Cosmos 1574

June 21, 1984

Decommissioned (June 1990)

965 x 1005, 83º

COSPAS-4

Nadezhda-1

July 4, 1989

Not in continuous operation

960 x 1014, 83º

COSPAS-5

Nadezhda-2

Feb. 27, 1990

Decommissioned (Feb. 1996)

956 x 1021, 83º

COSPAS-6

Nadezhda-3

Mar. 12, 1991

Decommissioned (Sept. 2001)

958 x 1018, 83º

COSPAS-7

Nadezhda-4

July 14, 1994

Decommissioned (July 1997)

954 x 1005, 83º

COSPAS-8

Nadezhda-5

Dec. 10, 1998

Decommissioned (Sept. 2001)

870 km, 98.74º

COSPAS-9

Nadezhda-6

Jun. 28, 2000

Decommissioned (Aug. 2007)
(121.5 MHz only)

686 x 712, 98.1º

COSPAS-10

Nadezhda-7

Sept. 26, 2002

Decommissioned (March 2004)
(called Nadezhda-M), start with SARP-2 configuration

987 x 1022, 83º

COSPAS-11

Sterkh-1

July 21, 2009

Replacement of the Nadezhda S/C series.
However, Sterkh 1 failed to properly align its solar panels with the sun due to a malfunction of the satellite's flight control system. Sterkh-2 failed to properly deploy its stabilization boom.

 

COSPAS-12

Sterkh-2

Sept. 17 2009

 

COSPAS-13

Sterkh-3

planned in 2012

 

 

COSPAS-14

Sterkh-4

planned in 2013

 

 

 

 

 

 

 

SARSAT-1

NOAA-8

Mar. 28, 1983

Decommissioned (Dec. 1985)

801 x 826, 98.2º

SARSAT-2

NOAA-9

Dec. 12, 1984

Decommissioned (Dec. 1997)
SARP not operational for 406 MHz

842 x 862, 98.9º

SARSAT-3

NOAA-10

Sept. 17, 1986

Decommissioned (Aug. 2001)

803 x 824, 98.7º

SARSAT-4

NOAA-11

Sept. 24, 1988

Decommissioned (June 16, 2004)

845 x 863, 98.9º

SARSAT-5

NOAA-13

Aug. 9, 1993

S/C failure 12 days after launch

 

SARSAT-6

NOAA-14

Dec. 30. 1994

Decommissioned on May 23, 2007

848 x 861, 98.9º

 

 

 

 

 

SARSAT-7

NOAA-15 (K)

May 13, 1998

Start with SARP-2 configuration
Operational of 406 MHz link
121.5/243 MHz processing ceased on 1 Feb. 2009

833 km, 98.86º

SARSAT-8

NOAA-16 (L)

Sept. 21,2001

Operational of 406 MHz link
121.5/243 MHz processing ceased on 1 Feb. 2009
SARSAT-8 was decommissioned on June 8, 2014.

 

SARSAT-9

NOAA-17 (M)

Jun. 24, 2002

Operational of 406 MHz link
121.5/243 MHz processing ceased on 1 Feb. 2009

 

SARSAT-10

NOAA-18 (N)

May 20, 2005

Operational of 406 MHz link
121.5/243 MHz processing ceased on 1 Feb. 2009

 

 

 

 

 

 

SARSAT-11

MetOp-A

Oct. 19, 2006

First installation of SARP-3 (2-way messaging services)
Operational of 406 MHz link
121.5/243 MHz processing ceased on 1 Feb. 2009

817 km, 98.7º

SARSAT-12

NOAA-19 (N')

Feb. 6, 2009

Operational since June 2009, 406 MHz link
SARP-3 with two-way messaging services

830 km, 98.6º

SARSAT-13

MetOp-B

Sept. 17, 2012

Operational since Jan. 29, 2013

817 km, 98.7º

 

 

 

 

 

GEO Satellites furnished with experimental Search and Rescue Equipment

GEOSAR

GOES-7

Feb. 26, 1987

First demonstration payload in GEO

 

GEOSAR

GOES-8

Apr. 13, 1994

GOES-8 was decommissioned on April 1, 2003

 

GEOSAR

GOES-9 (J)

May 23, 1995

Decommissioned on June 15, 2007
Since Apr. 2003, GOES-9 is providing backup service for GMS-5 of Japan, GOES-9 was decommissioned on June 15, 2007

155º E

GEOSAR

GOES-10 (K)

Apr. 25, 1997

Decommissioned in Dec. 2009 due to end-of-fuel

135º W

GEOSAR

GOES-11 (L)

May 3, 2000

Operational

135º W

GEOSAR

GOES-12 (M)

July 23, 2001

In standby since April 14, 2010
Will be drifted to 60º W in May 2010 to support users in South America

75º W

GEOSAR

GOES-13 (N)

May 24, 2006

Operational since April 14, 2010

105º W

GEOSAR

GOES-15 (P)

March 4, 2010

In-orbit storage

105º W

GEOSAR

Meteosat-8 (MSG-1)

Aug. 28 2002

Decommissioned on May 13, 2008

9.5º E

GEOSAR

Meteosat-9 (MSG-2)

Dec. 22, 2005

Operational in 2015

GEOSAR

Meteosat-10 (MSG-3)

July 05, 2012

Operational in 2015

 

GEOSAR

MSG-4

planned for 2015

 

 

 

 

 

 

 

SASAR

INSAT-2

July 9, 1992

Decommissioned

 

SASAR

INSAT-2B

July 22, 1993

Decommissioned in 2001, but still used for SASAR services

 

SASAR

INSAT-2C

Dec. 6, 1995

 

93.5º E

SASAR

INSAT-2D

June 3, 1997

S/C lost Earth lock in Oct. 1997

 

SASAR

INSAT-3A

Apr. 9, 2003

Operational, SASAR transponder in S-band

93.5º E

SASAR

INSAT-3D

July 25, 2013

INSAT-3D was declared operational on January 15, 2014

82º E

 

 

 

 

 

COSPAS

GOMS-1
(Electro-1)

Oct. 31, 1994

GOMS-1 mission operations were ended in Nov. 2000

76.5º E

GEOSAR

GOMS-2 (Electro-L)

Jan. 20, 2011

Nominal operations of Electro-L were started in January 2012.

76º E

GEOSAR

Luch-5A

Dec. 11, 2011

Russian GEO comminication satellite which features also a GEOSAR system

167º E

GEOSAR

Luch-5V

Apr. 28, 2014

Russian GEO comminication satellite which features also a GEOSAR system

 

 

 

 

 

 

MEO Satellites furnished with experimental Search and Rescue Equipment

SAR/Glonass

Glonass-K1 No 1

Feb. 26, 2011

First Glonass navigation satellite to carry an experimental MEOSAR payload on 3rd generation satellite

19,000 km altitude

SAR/Glonass

Glonass-K1 No 12L

Nov. 30, 2014 (UTC)

 

 

SAR/Galileo

VOV-3, IOV-4

Oct. 12, 2012

First Galileo navigation satellites of ESA carrying a MEOSAR payload

23,222 km altitude

SAR/Galileo

FOC-1, FOC-2

Aug. 22, 2014

A launch anomaly occurred and the operational capability of these satellites remains uncertain.

 

Table 3: Overview of SAR (Search & Rescue) payload launches

• MEOSAR operational payloads (with L-band downlink) will be mounted on three constellations of navigation satellites (Galileo, GPS III (9+), and Glonass K) providing more than 72 payloads in orbits after 2025.

• Today's MEOSAR Development and Evaluation (D&E) is made primarily via non-operational DASS payloads (S-band downlink) mounted on GPS II satellites. The DASS payloads will also be utilized for MEOSAR pre-operational use.

• 16 DASS POC payloads (S-band) are currently in orbit and an additional 12 payloads are expected to be deployed by 2019.

• Two L-band MEOSAR payloads (part of future operational system) are currently available for MEOSAR use, two on Glonass-K1 satellites and on the Galileo-IOV satellites. More Galileo FOC satellites are expected to be made available in 2015.

• Approximately 35 L-Band payloads are planned to be deployed for operational use by 2019.

Table 4: The Cospas-Sarsat MEOSAR Space Segment as of the end of 2014 31)

 


 

COSPAS-SARSAT Ground Segment:

The emergency signals are detected by the space segment (such as COSPAS-SARSAT) and relayed to LUTs which process the signals to determine beacon location. Alerts are then relayed, together with location data, via MCC (Mission Control Center) to the appropriate search and rescue point of contact or to RCC (Rescue Coordination Center).

Doppler location is the means used for signal location. The 406 MHz devices include an identification code in the alert message. Most 406 MHz devices also include a 121.5 MHz homing transmitter to support search and rescue operations. 32) 33) 34)

The 406 MHz emergency beacon signals are immediately processed and stored onboard the satellite and are transmitted to the ground from a continuous memory dump, providing complete worldwide coverage. Around the world, ground station LUTs (Local User Terminal) acquire the processed data and unique beacon identification and send these located and identified alerts to MCCs (Mission Control Centers), which forward the alerts to appropriate Rescue Coordination Centers for action. The 406 MHz beacons are designed to work well with the satellite; the system nominally provides better than 4 km accuracy, 90% ambiguity resolution on first pass, and better than 90% location probability on one pass. Note: the US SARSAT operational ground system facilities consist of SARSAT, SOCC at Suitland, MD as the MCC, and three LUTs. In addition to the US facilities, many other cooperating nations operate their own LUTs and MCCs.

The 121.5 MHz emergency beacons, whose use predates the satellite system, have not been specified to work with the satellite; consequently the results are variable, depending on the quality of the beacon. Nominally, location accuracy is about 20 km. All the processing is accomplished within the LUT, and because the satellite does not store these data, only beacons with mutual view of the satellite and LUT will be detected. No identification is included with the 125.5 MHz transmissions. Consequently, many nonbeacon sources are also detected as beacons, increasing the difficulty of using these alerts. Even with these problems, the large number of beacons in the field have provided an impressive performance history.

- The first rescue using Cospas-Sarsat took place near Dawson Creek, British Columbia, in September 1982 - just days after the first satellite was launched (June 1982). A pilot and two passengers were rescued from a plane crash. The signal was received using the world's first ground station, which was designed and built by Canadian industry and located at CRC (Communications Research Center).

- By the end of 2002, the COSPAS-SARSAT system had assisted in the rescue of over 15,700 persons in distress in about 4,500 SAR events (this includes maritime, aviation and land SAR events). About 100 people per month are rescued from distress situations ranging from plane crashes and boating accidents to hiking mishaps. 35)

- By the end of 2009, the COSPAS-SARSAT System had provided assistance in rescuing more than 27,000 persons in over 7,500 incidents (globally since 1982).

MCCs have been set up in most countries operating at least one LUT. Their main functions are to collect, store and sort the data from LUTs and other MCCs; provide data exchange within the Cospas-Sarsat System; and distribute alert and location data to associated RCC (Rescue Co-ordination Centers) or to SPOCs (SAR Points Of Contacts). In a nutshell, MCCs provide the distress alert and other related information to SAR authorities.

Basic tasks of MCCs (Mission Control Centers):

• Receive data from national LUTs and foreign MCCs

• Attempt to match signals coming from the same beacon source

• Merge beacon signals from the same source to improve location accuracy

• Geographically sort data to determine appropriate recipient of alert message

• Transmit alert messages to search and rescue authorities.

The initial MCCs of COSPAS-SARSAT system were provided by the agencies of the four founding countries who signed the MOU in 1979, namely the USSR (Russia), USA, France and Canada.

- CMC (Russian MCC, located in Moscow, Russia)

- USMCC (US MCC located at NOAA in Suitland, MD) 36)

- FMCC (French MCC located at CNES in Toulouse, France) 37)

- CMCC [Canadian MCC of DND (Department of National Defense) located in Trenton, Ontario]

The CMC and the USMCC distribute orbit ephemeris data for the COSPAS and SARSAT spacecraft daily. They automatically receive, process, confirm by their own calculations, and transmit the ephemeris data to the other MCCs and their own LUTs. - In 2010, there are about 30 MCCs distributed on a global scale.

 

LUTs (Local User Terminals):

There are various types of LUTs in the COSPAS-SARSAT ground system: 38)

1) LEOLUTs (Low Earth Orbit Local User Terminals): These operate with the LEOSAR payloads on the various spacecraft in orbit (of the USA, Russia, Europe, etc.)

2) GEOLUTs (Geosynchronous Earth Orbit Local User Terminals): These operate with the GEOSAR payloads flown on various GEO missions

3) MEOLUTs (Medium Earth Orbit Local User Terminals): These are the newest type (next generation) of LUTs in the definition/prototype phase as of 2008; they will be used to operate the future MEOSAR (Medium Earth Orbit Search and Rescue) payloads on the various navigation satellite constellations.

Basic tasks of LUTs:

• Track Cospas and Sarsat satellites

• Recover beacon signals from satellites

• Perform Doppler processing to determine geographic location

• Send resulting Doppler solutions to the associated MCC (Mission Control Center).

Cospas_AutoB

Figure 20: Locations of COSPAS-SARSAT LEOLUTs (April 2010), image credit: COSPAS-SARSAT

Cospas_AutoA

Figure 21: Legend to Figure 20 (image credit: COSPAS-SARSAT)

 


 

Satellite Payloads (GEO Space Segment)

The GEOSAR system consists of 406 MHz repeaters carried on board various geostationary satellites, and the associated ground facilities, called GEOLUTs, which process the satellite signal. As of 2008, the GEOSAR system is composed of the following spacecraft: 2 GOES satellites of NOAA, MSG-1 (Meteosat-8) of EUMETSAT, and INSAT-3A of ISRO.

GEOSAR (Geostationary Search and Rescue)

With the launch of GOES-H (GOES-7) on Feb. 26 1987, NOAA has started to introduce the SARSAT payload also on its geostationary satellites (406 MHz beacon). The use of geostationary satellites means that the alert signals can be received almost instantly. However, in order to automatically determine the coordinates of the emergency signal, it is necessary to wait for the system's LEO satellite (position determination can only be provided from a system that moves relative to the Earth).
Note: A satellite in GEO remains fixed with respect to an observer on Earth; hence, there is no relative motion between the satellite and the distress beacon in the GEOSAR system - with the consequence of no Doppler shift to automatically locate the beacon. 39)

The GEOSAR system concept thus works in two stages. In the first stage only the emergency signal is received via the geostationary satellite (it is planned to equip GMS and GOMS satellites for this service as well). The received alert signal is transmitted to the search and rescue service to prepare for the operation. In the second stage, the site of the signal origin is determined by the SAR payload on the nearest LEO satellite.

In addition, the capability exists for 406 MHz beacons to encode location information derived from a satellite navigation receiver, such as GPS, Glonass or the future Galileo system, and to transmit this location data along with the beacon identification code.

 

SASAR (Satellite Aided Search and Rescue)

ISRO (Indian Space Research Organization), Bangalore, India, has introduced the "COSPAS-SARSAT" prototype service in 1992 with its SASAR (Satellite Aided Search and Rescue) demonstration payload flown on the GEO INSAT-2 series, starting with INSAT-2A (launch July 9, 1992). Alert messages of the 406 MHz beacon in the ground segment are being received and relayed by the SASAR system.

Based on the performance demonstrations of INSAT, the SASAR system has now been adopted (2004) as an integral part of the international COSPAS-SARSAT system for satellite-aided search and rescue operations complementing the LEOSAR system. 40)

The INSAT-GEOSAR Local User Terminal (GEOLUT), located at Bangalore, is integrated with INMCC (INSAT Mission Control Center). The distress alert messages originating from the Indian service area are detected at INMCC which are passed on to Indian Coast Guard and Rescue Coordination Centers (RCCs) at Mumbai, Kolkata, Delhi and Chennai. Coast Guard, Navy and Air Force carry out the search and rescue activities. The INMCC is linked to the RCCs and other international MCCs through automatic telex and Aeronautical Fixed Telecommunication Network (AFTN). The Indian LUTs and MCC provide service round the clock and maintain the data base of all 406 MHz registered beacons equipped on Indian ships and aircraft. 41)

 


 

Next Generation Satellite Payloads in the MEO (Medium Earth Orbit) Space Segment

The future of COSPAS-SARSAT will be realized through the third phase of development, based on a Medium Earth Orbit Search and Rescue (MEOSAR) system. These new MEOSAR services are being planned by the three navigation system constellations: GPS (USA), GLONASS (Russia), and Galileo (Europe)- also referred to as GNSS (Global Navigation Satellite Systems). The three potential MEOSAR providers have confirmed that their systems would be fully compatible with existing COSPAS-SARSAT beacons of 406 MHz (this includes also new beacon designs with improved capabilities). The density of all the satellites in the three constellations offer the potential of practically immediate (real-time and continuous) alert recognition. It is also planned to use the future beacons with "return link" capability. 42) 43) 44) 45) 46) 47)

All GNSS (Global Navigation Satellite System) satellites feature orbits of about 20,000-23,000 km altitude in various orbital planes with periods of about 12 hours (half a day). Hence, MEO orbits provide considerably longer contact times with the user on Earth's surface, as well as larger footprints than spacecraft in LEO. For the planned MEOSAR payloads on GNSS, it implies that the Doppler shift of 406 MHz beacons will be considerably smaller (than the one experienced on LEOSAR systems), resulting in a reduced location identification capability. On the other hand, the dense future GNSS network (starting from about 2010 onwards) implies, that alert signals from anywhere on Earth will be received simultaneously by several GNSS satellites, thus permitting precise location identification by triangulation algorithms.

The USA MEOSAR program is called the DASS (Distress Alerting Satellite System), Russia's program is called SAR/GLONASS, and the EC program is named SAR/Galileo. In July 2006, the Canadian Government offered to NASA to provide DASS (Distress Alerting Satellite System) transponders for GPS-III series satellites as a continuation of their national contribution to the COSPAS-SARSAT Program. 48)

The ground system of each MEOSAR system implementation will feature MEOLUTs (MEO Local User Terminals) which will be connected to the existing MCCs (Mission Control Centers) of the respective systems (DASS, SAR/GLONASS, SAR/Galileo). 49) 50) 51)

 

Background: In 2000 the United States, the European Commission (EC) and Russia began consultations with Cospas-Sarsat regarding the feasibility of installing 406 MHz SAR instruments on their medium-altitude Earth orbiting (MEO) GPS, Galileo, and GLONASS navigation satellite systems. These MEOSAR constellations—DASS, SAR/Galileo, and SAR/GLONASS—eventually could become components of a 406 MHz Cospas-Sarsat MEOSAR system.

In 2006, the Canadian government offered to provide the DASS transponders for GPS-III satellites as a continuation of their national contribution to the COSPAS-SARSAT program. The payload will be functionally similar to the POC (Proof-Of-Concept) system, though the downlink will operate at 1544 MHz instead of S-band. The system will operate as an independent GPS-III payload.

MEOSAR overcomes the limitations of the current COSPAS-SARSAT system based on satellites that are either in GEO or in LEO. MEOSAR provides visibility of a large portion of Earth's surface and, because of the large number of satellites in each constellation, will be able to to provide near-instantaneous detection, identification, receipt of encoded position, and independent localization of distress beacons. Moreover, since the MEOSAR allows handling of multiple signal paths, the detection and tracking of beacons should become more efficient. Distress calls being located almost instantaneously should allow tracking moving vessels or airplanes in distress.

For the MEOSAR constellations, there is also the capability that the system will be able to return information back to the distress radiobeacon initiator via the MEOSAR downlink. Confirmation to the person in distress - that their distress alert has been received - might improve their morale, thus enhancing their chances for survival. - MEOSAR operational alerts could be available (i.e. start their service) in the timeframe 2014-2016.

The elements of the MEOSAR system are being developed by various agencies/entities:

• Space Segment (GPS, Glonass and Galileo)

• Ground Segment (USA, Canada, Europe, Russia, China, India, etc.). The MEOLUTs (MEO Local User Terminals) are in charge of recovering the message and locating the emergency beacon.

• Beacons: existing 406 MHz beacons will work with MEOSAR, but studies are underway to improve the future beacons.

Cospas_Auto9

Figure 22: Comparison of LEO and MEO footprints (image credit: CRC, Canada)

Cospas_Auto8

Figure 23: Overview of the MEOSAR system concept within GNSS (image credit: ISU Symposium 2010, Strasbourg, Ref. 7)

SAR (Search and Rescue) demonstrations from MEO orbits have up to now (2010) been attempted only on a proof-of-concept (POC) basis, utilizing a number of GPS block-II satellites with not-fully-representative SAR payloads. The POC concept trials are based on a number of S-band transponders with on-orbit trials being performed by all Cospas-Sarsat Parties, the RLS (Return Link Service) has not been demonstrated in orbit as yet.

 

DASS (Distress Alerting Satellite System):

When DASS first becomes operational, the space segment will be hosted aboard GPS-III satellites. The operational DASS system will include 406 MHz repeaters (transponders) on all GPS satellites. The operational transponders will use downlinks in the 1544-1545 MHz band (L-band).

The DASS proof-of-concept (POC) and demonstration will be conducted using transponders with S-band downlinks. The DASS POC payloads will operate aboard nine GPS Block-IIR and all Block-IIF satellites. They will use an existing GPS capability to minimize impact to the satellites prior to full fielding of DASS. Beacon signals, without any processing aboard the satellites, will be relayed to the MEOLUT through an existing S-band antenna (2226.42 – 2226.52 MHz). The future operational link will be L-band, a frequency internationally-recognized frequency for this purpose. 52)

The US primary partner agencies involved in the development of DASS are: NASA, NOAA, USAF, and USCG (US Coast Guard). NASA leads DASS planning, development, and proof-of-concept testing efforts. Upon transition to an operational system, DASS is expected to be managed and operationally funded by NOAA, the USAF, and the USCG. 53)

GPS-SAR (GPS Search and Rescue): The GPS-III SAR (Search & Rescue) payload began as the proof-of-concept DASS (Distress Alerting Satellite System), it uses an S-band downlink and was developed by the NASA SAR Mission Office in partnership with the DoD and SNL (Sandia National Laboratory) in support of the NSARC (National SAR Committee) and successfully implemented on GPS -IIR(M), and -IIF space vehicles (Figure 4). NASA has invested about $35M to develop the POC DASS. The operational version of DASS, renamed GPS-SAR (GPS Search and Rescue), is planned for the GPS III constellation starting with Space Vehicle 9 for launch in the 2019 timeframe. Canada is funding and providing the search-and-rescue repeaters for GPS III. GPS-SAR will provide: 406 MHz ‘bent pipe' repeaters on future GPS satellites; full compatibility with existing and future 406 MHz beacons; and global near-instantaneous detection and location. 54)

Cospas_Auto7

Figure 24: Proof-of-concept DASS (image credit: NASA)

Future GPS SAR development could potentially provide additional capabilities such as: a digital message return confirmation message; aids in false alarm mitigation; direct communications with survivors; support rescue force coordination; and reduced interference susceptibility via confirmation.

Cospas_Auto6

Figure 25: MEOSAR / DASS overview (image credit: NOAA, Ref. 51)

Cospas_Auto5

Figure 26: US MEOSAR ground segment design (image credit: NOAA)

 

SAR/Galileo (Search and Rescue Service / Galileo constellation):

The SAR/Galileo system will provide two services to improve the time to detection and the accuracy of location of distress beacons over the current COSPAS/SARSAT system in LEO:

- FLS (Forward Link Service) - also known as the 'alert service'

- RLS (Return Link Service).

Whereas the forward link based service can be seen as an upgrade of the currently operational LEO and GEO equivalents, Galileo foresees in addition to include a new service, the RLS , which will provide the user in distress with a confirmation that its call for help has been received and that aid is underway.

The unprecedented service levels in terms of distress localization accuracy and response time are obtained by the innovative algorithms developed within the European MEOLUT station on ground, which is connected to the associated COSPAS-SARSAT MCC (Mission Control Centre) which in turn will eventually launch the rescue operations.

The RLS (Return Link Service) relays Return Link Messages from the RLSP (Return Link Service Provider) to new generation beacons through the Galileo navigation signal. The RLS provides technical acknowledgments, after successful detection and localization of an active beacon, and operational acknowledgements after the deployment of a rescue team. 55)

Cospas_Auto4

Figure 27: SAR/Galileo system architecture (image credit: ESA, Indra Espacio)

The approach of the SAR/Galileo program is the use of a comprehensive SAR-VTB (Search and Rescue Service - Validation Test Bench), within the context of the Galileo FOC (Full Operational Capability) system tools procurement, which comprises the procurement of a wide range of tools for performance evaluation, test benches, signal monitoring facilities and simulation facilities. Actually, two versions of the SAR-VTB facility are foreseen to be developed and integrated, to experiment with the IOV (In-Orbit Validation) and FOC Galileo configurations, respectively. 56)

The C/S POC (COSPAS/SARSAT Proof-Of-Concept) will eventually become the C/S D&E (Demonstrator & Evaluation) system, then the C/S IOV (In-Orbit Validation), and lastly the C/S FOC (Full Operational Capability) system as shown in Figure 28. The SAR-VTB shall be able to operate independently of the operational COSPAS-SARSAT system, using the COSPAS-SARSAT Network Emulator, but shall be capable of interfacing with it (LUT-to-MCC and nodal-MCC -to-RLSP).

The SAR-VTB is based on a number of modules developed in or for the IOV phase of the GALILEO project. The SAR elements to be considered for integration into the SAR-VTB include existing developments. These include the elements developed in the GISAR (Galileo Interfaces for SAR).

Cospas_Auto3

Figure 28: SAR/Galileo as part of the MEOSAR system (image credit: ESA)

The European MEOLUT SAR/Galileo prototype station has been developed under the GISAR (Galileo Interfaces for Search and Rescue) implementation contract FP6 (Sixth Framework Program) of the EU and its installation realized at the CNES Toulouse site (France).57)

GISAR (or GISAR) provides the following features:

• Satellite tracking, up to 4 satellites

• Signal In Space acquisition in SAR/Galileo downlink band (1544.05 – 1544.15 MHz) and DASS POC band (2226.42 – 2226.52 MHz)

• Beacon message demodulation

• TOA/FOA (Time of Arrival/Frequency of Arrival) measurement with high accuracy

• SAR beacon localization

• Interface with MCC.

Cospas_Auto2

Figure 29: SAR-VTB in the first stage - components and interfaces overview (image credit: ESA)

Cospas_Auto1

Figure 30: SAR-VTB in final stage (image credit: ESA)

• In October 2013, ESA completed a pair of dedicated ground stations at opposite ends of Europe. This enabled the first Galileo satellites in MEO to participate in global testing of the COSPAS–SARSAT (S&RSAT) search and rescue system. - The Maspalomas station, at the southern end of the largest island of the Canary Islands, at the southern fringe of European waters, was activated in June 2013. And this last month has seen the Svalbard site on Spitsbergen in the Norwegian Arctic come on line — the two sites can already communicate and willsoon be performing joint tests. 58)

Founded by Canada, France, Russia and the US, COSPAS–SARSat has assisted in the rescue of tens of thousands of souls in its three decades of service. Distress signals from across the globe are detected by satellites, then swiftly relayed to the nearest search and rescue (SAR) authorities.

Cospas_Auto0

Figure 31: Photo of the MEOLUT (MEO Local User Terminal) at the Maspalomas station (image credit: ESA)

The Galileo satellites, tested in combination with the same SAR payloads on Russian Glonass satellites as well as compatible repeaters on a pair of US GPS satellites, showed an ability to pinpoint simulated emergency beacons down to an accuracy of 2–5 km in a matter of minutes. Maspalomas and Spitsbergen will combine with a third station at Larnaca in Cyprus, currently approaching completion. These three sites are monitored and controlled from the SAR Ground Segment Data Service Provider site, based at Toulouse in France.

Each site is equipped with four antennas to track four satellites. The stations are networked to share raw data, effectively acting as a single huge 12-antenna station, achieving unprecedented detection time and localisation accuracy.

 


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The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: "Observation of the Earth and Its Environment: Survey of Missions and Sensors" (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002. - Comments and corrections to this article are always welcome for further updates (herb.kramer@gmx.net).

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