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TRIMIS

Navigation of Airborne Vehicle with Integrated Space and Atomic Signals

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€890 910
EU Contribution
€584 979
Project Acronym
NAVISAS
STRIA Roadmaps
Connected and automated transport (CAT)
Network and traffic management systems (NTM)
Transport mode
Airborne icon
Transport policies
Other specified
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-SESAR-2015-1
Link to CORDIS
Background & Policy context

Global Navigation Satellite System Positioning, Navigation and Timing (PNT) services have been increasing the airspace capacity, efficiency and safety and continue to proliferate and support more and more performance-based navigation operations. In the event of GNSS interference or outage, many GNSS enabled PNT services will be lost and the existing legacy navigation aids (VOR, DME, NDB and Secondary Radar) do not meet performance requirements nor maintain adequate capacity and efficiency. Therefore, a disruption to air traffic operations is expected to occur.

Due to this disturbing reality and considering the growth of the worldwide air traffic, continuous, robust/resilient and high precision alternative positioning, navigation and timing (APNT) services and technologies are needed to maintain flight operations with the required level of performance while ensuring safety and security.

Current solutions for APNT comprise of ground-based infrastructures transmitting non-GNSS signals-in-space to avionics. However, all these solutions cannot be used by small aircraft without major reengineering of their avionic systems.

Objectives

The NAVISAS Consortium will propose a novel concept of APNT for small aircraft that will integrate novel technologies and will merge multiple navigation avionics into one with no major impact on avionics. Specifically, NAVISAS is devoted to combine multiple GNSS constellations (GLONASS, GPS and Galileo) and a novel concept of atomic micro-gyroscope based on atomic spin and nuclear magnetic moment precessions, and to assess the improvements in performance and security. The technology of these gyros relies on a similar cell used for miniature atomic clocks, and will allow bridging the gap between the price of navigation grade gyroscopes and the market constraints for affordable non-inertial navigation systems and avionics in small aircraft, thus contributing significantly to enhancement of the flight safety level.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.7.1

Partners

Lead Organisation
Organisation
Tekever - Tecnologias De Informacao, S.a.
Address
RUA DA LEZIRIA 1, 2510 219 OBIDOS, Portugal
Organisation website
EU Contribution
€374 000
Partner Organisations
Organisation
Shark.aero S.r.o
Address
LETISKO SENICA HLBOKE 406, 906 31 HLBOKE, Slovakia
EU Contribution
€117 188
Organisation
Csem Centre Suisse D'electronique Et De Microtechnique Sa - Recherche Et Developpement
Address
Rue Jaquet Droz 1, 2002 Neuchatel, Switzerland
EU Contribution
€0
Organisation
Thales Avs France Sas
Address
75-77 Avenue Marcel Dassault, 33700 Merignac, France
EU Contribution
€93 791

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Guidance, Navigation & Control technologies
Development phase
Research/Invention

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