A H control solution for space debris removal missions using robotic arms: the ESA e.Deorbit case

Author:

Faure M.1,Henry D.1,Cieslak J.1,Colmenarejo P.2,Ankersen F.3

Affiliation:

1. Univ. Bordeaux, Bordeaux INP, CNRS (UMR 5218),IMS Lab.,Talence,France,33405

2. GMV,Madrid,Spain,E-28760

3. European Space Agency,AG Noordwijk,Netherlands,2200

Funder

European Space Agency

Publisher

IEEE

Reference26 articles.

1. Essentials of robust control;zhou,1999

2. A necessary and sufficient minimality condition for uncertain systems

3. Satellite collision leaves significant debris clouds;NASA Orbital Debris Quarterly News,2009

4. Methods and outcomes of the COMRADE project - design of robust coupled control for robotic spacecraft in servicing missions: trade-off between H? and nonlinear lyapunov-based approaches;colmenarejo;International Astronautical Congress,2018

5. Definition of an automated vehicle with autonomous fail-safe reaction behavior to capture and deorbit Envisat;estable;7th European Conference on Space Debris,2017

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