FADER

Flight Algorithms for Disaggregated Space Architectures

 Coordinatore TECHNION - ISRAEL INSTITUTE OF TECHNOLOGY 

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 Nazionalità Coordinatore Israel [IL]
 Totale costo 1˙499˙999 €
 EC contributo 1˙499˙999 €
 Programma FP7-IDEAS-ERC
Specific programme: "Ideas" implementing the Seventh Framework Programme of the European Community for research, technological development and demonstration activities (2007 to 2013)
 Code Call ERC-2011-StG_20101014
 Funding Scheme ERC-SG
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-10-01   -   2016-09-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    TECHNION - ISRAEL INSTITUTE OF TECHNOLOGY

 Organization address address: TECHNION CITY - SENATE BUILDING
city: HAIFA
postcode: 32000

contact info
Titolo: Mr.
Nome: Mark
Cognome: Davison
Email: send email
Telefono: +972 4 823 3097
Fax: +972 4 823 2958

IL (HAIFA) hostInstitution 1˙499˙999.60
2    TECHNION - ISRAEL INSTITUTE OF TECHNOLOGY

 Organization address address: TECHNION CITY - SENATE BUILDING
city: HAIFA
postcode: 32000

contact info
Titolo: Prof.
Nome: Pinchas Pini
Cognome: Gurfil
Email: send email
Telefono: +972 4 829 4973
Fax: +972 4 829 5643

IL (HAIFA) hostInstitution 1˙499˙999.60

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

modules    space    algorithms    cluster    autonomous    module    spacecraft    attitude    disaggregated    dsa    network    single    semi    termed    payload    flying    architectures   

 Obiettivo del progetto (Objective)

'Standard spacecraft designs comprise modules assembled in a single monolithic structure. When unexpected situations occur, the spacecraft are unable to adequately respond, and significant functional and financial losses are unavoidable. For instance, if the payload of a spacecraft fails, the whole system becomes unserviceable and substitution of the entire spacecraft is required. It would be much easier to replace the payload module only than launch a completely new satellite. This idea gives rise to an emerging concept in space engineering termed disaggregated spacecraft. Disaggregated space architectures (DSA) consist of several physically-separated modules, interacting through wireless communication links to form a single virtual platform. Each module has one or more pre-determined functions: Navigation, attitude control, power generation and payload operation. The free-flying modules, capable of resource sharing, do not have to operate in a tightly-controlled formation, but are rather required to remain in bounded relative position and attitude, termed cluster flying. DSA enables novel space system architectures, which are expected to be much more efficient, adaptable, robust and responsive. The main goal of the proposed research is to develop beyond the state-of-the-art technologies in order to enable operational flight of DSA, by (i) developing algorithms for semi-autonomous long-duration maintenance of a cluster and cluster network, capable of adding and removing spacecraft modules to/from the cluster and cluster network; (ii) finding methods so as to autonomously reconfigure the cluster to retain safety- and mission-critical functionality in the face of network degradation or component failures; (iii) designing semi-autonomous cluster scatter and re-gather maneuvesr to rapidly evade a debris-like threat; and (iv) validating the said algorithms and methods in the Distributed Space Systems Laboratory in which the PI serves as a Principal Investigator.'

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