Alphasat Aldo Paraboni payload IOT campaign and status after the first year of operation

Summary The use of higher frequencies for satellite multimedia communication systems calls for research of the atmospheric propagation effects at these bands (rain, cloud and gaseous attenuation, scintillation, and depolarization). Alphasat was successfully launched on 25 July 2013. This largest and most powerful European telecommunication satellite carries, besides a commercial payload belonging to the mobile satellite communication provider Inmarsat, several Technology Demonstration Payloads (TDPs) from ESA. One of them is the Aldo Paraboni payload (TDP5) for Q/V‐band communication and Ka/Q‐band propagation experiments. These experiments explore future applications in satellite communication and measure how the Earth's atmosphere affects the propagation of electromagnetic waves. Under ESA contract, JOANNEUM RESEARCH designed, developed, and operates a Q/V‐band communication ground station and a Ka/Q‐band propagation terminal. The experimental site is equipped with ancillary equipment including a multifrequency radiometer profiler, a 2D video disdrometer (2DVD), and meteorological stations. This paper reports on the experimental setup, data processing, and obtained results.

Section: Alphasat Aldo Paraboni Payload Iot Campaignmentioning

confidence: 58%

The Alphasat Aldo Paraboni scientific and communication experiments at Ka and Q/V bands in Austria

Cuervo

Martellucci

Castro

et al. 2019

Section: Discussionmentioning

confidence: 99%

“…Achieved results and the experience acquired from the Aldo Paraboni Payload operation within the Q/V band program will allow a more effective use of the Q/V spectrum and provide a fundamental contribution to the development of future HTS systems. 13,14 In particular, the architecture of the Aldo Paraboni Payload IMS was presented with an overview at system level and with the description of main components, their interaction and operational features.…”

Section: System Functional and Performance Test-first Stepmentioning

confidence: 99%

Alphasat Aldo Paraboni Payload Italian mission segment

Cornacchini

Bernardo

Falzini

et al. 2018

Summary In the framework of the ASI Q/V band program, the “Aldo Paraboni” Payload embarked on Alphasat is devoted to the exploitation and the investigation on communications at the Q/V frequency band. The operation of this experimental payload allowed to demonstrate the potential of advanced broadband satellite communications at the Q/V frequency bands and represents an important step toward the development of future High Throughput Satellite (HTS) systems. The Italian Mission Segment (IMS) represents the ground infrastructure which allows to perform communications experiments (propagation impairment mitigation techniques (PIMT)) at 40/50 GHz (Q/V band) and propagation experiments at both 20 GHz (Ka band) and 40 GHz (Q band) by operating the Aldo Paraboni Payload. The IMS was developed under the Italian Space Agency contract and developed by the Italian industry in accordance with the requirements defined for communications and propagation experiments by two principal investigators, appointed by the Italian Space Agency. The IMS consists of two transmitting/receiving ground stations and three control centers, while the space segment is represented by the Aldo Paraboni Payload, financed by Italy through the ARTES‐8 Program, developed by the European Space Agency and implemented by Italian space industries. The Aldo Paraboni Payload, also called technology demonstration payload #5 (TDP#5), has been embarked as piggyback on Alphasat satellite, an INMARSAT Commercial Telecommunication Geosynchronous satellite successfully launched on 25 July 2013, which uses the ESA‐developed Alphabus Platform and embarks other four technology demonstration payloads (TDPs). This paper presents an overview of the overall system composing the IMS, the functional architecture, main subsystems, and specific features related to the communication and propagation experiments. The ground station validation is also described, together with the description of the system test campaign, performed for functional and performance verification of the IMS. The campaign allowed to test the Q/V band communication functions and to perform the propagation experiment verification, operating the payload in loopback mode and in cross mode.

“…The in-flight performances were measured after the launch, during the In-Orbit Test (IOT) campaign (see 9,10 ). These performances have been regularly monitored during operations by repeating regularly a reduced set of the IOT procedures in a series of min-IOT campaigns.…”

Section: Payload Architecturementioning

confidence: 99%

Alphasat Aldo Paraboni, an advanced Q/V band mission space segment

Rivera

Martellucci

Sivac

et al. 2019

Summary This paper provides an overview of the space segment of the Aldo Paraboni mission on the Alphasat satellite and the technology programme that has developed one of the most powerful geostationary satellites in Europe. The Aldo Paraboni technology demonstration payload, funded by ASI under European Space Agency's Advanced Research in Telecommunications System Programme, was embarked as a hosted payload on the Alphasat satellite, launched on 25 July 2013. The Aldo Paraboni payload is composed of two main elements, an experimental communication payload operating at Q/V bands (COMEX) and a scientific payload formed by 2 beacons at Ka and Q bands (SCIEX). The Aldo Paraboni payload is a key technology element of the Aldo Paraboni Mission, which covers two main objectives: the communication segment of the mission aims at assessing the performance of satellite communication links at Q/V bands and investigating use Fade Mitigation Techniques (FMT, eg, Adaptive Coding and Modulation defined in DVB‐S2 standard), while the scientific segment aims at characterizing in time, space, and frequency the K and Q band radio channel over Europe to permit development and improvement of propagation channels for slant paths.