Trajectory planning/re-planning for satellite systems in rendezvous mission in the presence of actuator faults based on attainable efforts analysis
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Publication:5265645
DOI10.1080/00207721.2013.797034zbMath1316.93086OpenAlexW2127916750MaRDI QIDQ5265645
Abbas Chamseddine, Didier Theilliol, Cédric Join
Publication date: 28 July 2015
Published in: International Journal of Systems Science (Search for Journal in Brave)
Full work available at URL: https://hal.inria.fr/hal-00831637/file/Paper_WWW.pdf
Application models in control theory (93C95) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)
Related Items (2)
Hybrid multi-objective optimisation for concurrent activities consolidating two docked spacecraft ⋮ Active fault-tolerant control system design with trajectory re-planning against actuator faults and saturation: Application to a quadrotor unmanned aerial vehicle
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