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SAT STABILIS

Nonlinear Sampled-data Attitude Stabilization of Underactuated Spacecraft

Total Cost €

0

EC-Contrib. €

0

Partnership

0

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 SAT STABILIS project word cloud

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

reliability    stakeholders    hoc    simulations    momenta    feedback    nonholonomic    never    fail    minimum    demonstration    admitting    assured    restrictions    safe    discrete    varying    continuous    operation    space    software    angular    classes    symmetricity    global    underactuated    degradation    laws    torques    secondment    platform    spacecraft    innovative    remaining    experimental    foreseen    digitally    impose    nonlinear    algorithms    beginning    computer    market    ad    finite    solutions    permitting    theoretical    controller    investigations    sampled    stabilizing    small    effect    extensive    attitude    dictated    orbit    industrial    models    sampling    discontinuous    board    manifest    applicability    mode    additional    though    purpose    multirate    redundancy    depending    outcomes    mechanical    time    axis    equivalent    performance    quality    follow    kept    actuator    inevitably    digital    standard    smooth    data    destabilization    stabilization    methodology    underlying    computability    satellites   

Project "SAT STABILIS" data sheet

The following table provides information about the project.

Coordinator
UNIVERSITA DEGLI STUDI DI ROMA LA SAPIENZA 

Organization address
address: Piazzale Aldo Moro 5
city: ROMA
postcode: 185
website: www.uniroma1.it

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.dis.uniroma1.it/
 Total cost 180˙277 €
 EC max contribution 180˙277 € (100%)
 Programme 1. H2020-EU.1.3.2. (Nurturing excellence by means of cross-border and cross-sector mobility)
 Code Call H2020-MSCA-IF-2014
 Funding Scheme MSCA-IF-EF-CAR
 Starting year 2015
 Duration (year-month-day) from 2015-10-01   to  2017-09-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    UNIVERSITA DEGLI STUDI DI ROMA LA SAPIENZA IT (ROMA) coordinator 180˙277.00

Map

 Project objective

Space stakeholders manifest an increasing interest in small satellites dictated by reduced, global costs and “time to market”. Since redundancy is kept to a minimum, achieving attitude stabilization in actuator failure mode with the remaining control torques can offer a fail-safe operation mode, improving the reliability of the attitude control system. The, still open, underlying control problem is challenging, since the nonlinear underactuated system is nonholonomic, admitting only non-smooth stabilizing feedback. Depending on actuator type and additional restrictions on the symmetricity of the spacecraft or its angular momenta, non standard, discontinuous or time-varying solutions have been proposed. Though any continuous-time controller is inevitably implemented digitally on the on-board computer, leading to loss of performance or even destabilization, the effect of sampling is never considered in the state-of-the-art. The aim of the present proposal is to develop novel control algorithms for three-axis attitude stabilization of an underactuated spacecraft in actuator failure mode without significant performance degradation with the remaining control torques. To this purpose, we follow a sampled-data methodology that considers the sampling issues from the beginning in the design process. Theoretical investigations will be conducted for ad-hoc digital solutions based on equivalent discrete models, finite computability and multirate control laws, permitting to impose digital performance objectives that cannot be set in continuous-time. The quality of the innovative algorithms developed is assured by extensive software simulations and application on an experimental attitude control platform. In-orbit technology demonstration and testing, and exploitation of the research outcomes are the focus of the industrial secondment foreseen. The applicability of the results to general classes of underactuated mechanical systems and other related control problems is expected.

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

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