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Opendata, web and dolomites

PALADIN

Plasma Antenna for secure LAnDIng and Navigation

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

PALADIN project word cloud

Explore the words cloud of the PALADIN project. It provides you a very rough idea of what is the project "PALADIN" about.

aviation either track position solution null former preliminary operation free commercial drag algorithms lobes update accuracy interference discharges performance board satellite smart pattern software structure electronically antennas thanks electromagnetic lobe landing market aircraft paladin tracked positioning proficiently steering lock dsp operations simulation nulls gnss reflections industrialization tuneable regard reference plasma exploits signal interferences narrow evaluation critical reconfigurable secure business prototyping latter gbas noise feasibility create integrate spoofing satellites ratio preparation beamwidth directions wing antenna navigation ground technologies place replacing resistant radiation actual plan estimation jamming

Project "PALADIN" data sheet

The following table provides information about the project.

Coordinator	ALMA SISTEMI SRL Organization address address: VIA DEI NASTURZI 4 city: GUIDONIA MONTECELIO RM postcode: 12 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	Italy [IT]
Project website	http://www.alma-sistemi.com
Total cost	71˙429 €
EC max contribution	50˙000 € (70%)
Programme	1. H2020-EU.2.1.6. (INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies – Space) 2. H2020-EU.2.3.1. (Mainstreaming SME support, especially through a dedicated instrument)
Code Call	H2020-SMEINST-1-2015
Funding Scheme	SME-1
Starting year	2015
Duration (year-month-day)	from 2015-07-01 to 2015-12-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	ALMA SISTEMI SRL ALMA SISTEMI SRL Organization address address: VIA DEI NASTURZI 4 city: GUIDONIA MONTECELIO RM postcode: 12 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (GUIDONIA MONTECELIO RM)	coordinator	50˙000.00
2	LTG ELETTRONICA S.R.L. LTG ELETTRONICA S.R.L. Organization address address: LARGO BIANTE 10 city: ROMA postcode: 124 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (ROMA)	participant	0.00
3	TECHNOLOGY FOR PROPULSION AND INNOVATION SRL TECHNOLOGY FOR PROPULSION AND INNOVATION SRL Organization address address: VIA ALTINATE 125 city: PADOVA postcode: 35121 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (PADOVA)	participant	0.00

Map

Project objective

The PALADIN antenna exploits the electronically reconfigurable features of several plasma discharges along with DSP algorithms to create narrow beamwidth and multi-lobes radiation pattern. These features allows the PALADIN antenna to lock and track up to 4 navigation satellites (each lobe for a distinct satellite) to achieve higher signal to noise ratio, and to create nulls in the directions of electromagnetic interference including jamming, spoofing and multi-path reflections. Such features can be proficiently adopted either on board of an aircraft or on the ground replacing GBAS reference antennas. In the former case, the antenna can be embedded in the wing structure providing a drag-free solution, which can achieve better accuracy in position estimation thanks to the many GNSS satellites being tracked, and can integrate different antenna into one solution thanks to the tuneable properties offered by plasma discharges. In the latter case, the antenna can be used in place of actual landing system reference antennas thanks to its null steering in the directions of interferences and jamming resistant operations. The proposed study project PALADIN has the following high-level objectives: 1) Technical Assessment of the technology addressing antenna design and simulation; 2) Exploitation plan including commercial feasibility, business plan and preparation of Phase 2 activities. Technical assessment will focus in the update of the existing simulation software for plasma antenna performance evaluation and the design of a Smart Plasma Antenna for secure landing and navigation operation. Technical assessment will also include the evaluation of critical technologies required for prototyping and industrialization. Commercial Feasibility and Business Plan will provide a preliminary market assessment and positioning of the expected product with specific regard to aviation and the preparation of phase 2 activities.

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The information about "PALADIN" are provided by the European Opendata Portal: CORDIS opendata.