Validated simulator for space debris removal with nets and other flexible tethers applications

• Published in: Acta astronautica Vol. 129; pp. 229 - 240
• Main Authors: Gołębiowski, Wojciech, Michalczyk, Rafał, Dyrek, Michał, Battista, Umberto, Wormnes, Kjetil
• Format: Journal Article
• Language: English
• Published: Elmsford Elsevier Ltd 01.12.2016; Elsevier BV
• Subjects: Aircraft components; Cages; Computer simulation; Damping; Design; Detritus; Dynamics; Elastic bodies; Elasticity; Flexible bodies; Mathematical models; Microgravity; Mission planning; Parabolic flight; Rigid structures; Satellites; Simulation; Software; Space debris; Space debris mitigation; Space exploration; Tethers; Topology; Trajectories; Trusses; ANW, Canada; Canada, Ontario, Ottawa
• ISSN: 0094-5765; 1879-2030
• DOI: 10.1016/j.actaastro.2016.08.037

In the context of active debris removal technologies and preparation activities for the e.Deorbit mission, a simulator for net-shaped elastic bodies dynamics and their interactions with rigid bodies, has been developed. Its main application is to aid net design and test scenarios for space debris deorbitation. The simulator can model all the phases of the debris capturing process: net launch, flight and wrapping around the target. It handles coupled simulation of rigid and flexible bodies dynamics. Flexible bodies were implemented using Cosserat rods model. It allows to simulate flexible threads or wires with elasticity and damping for stretching, bending and torsion. Threads may be combined into structures of any topology, so the software is able to simulate nets, pure tethers, tether bundles, cages, trusses, etc. Full contact dynamics was implemented. Programmatic interaction with simulation is possible – i.e. for control implementation. The underlying model has been experimentally validated and due to significant gravity influence, experiment had to be performed in microgravity conditions. Validation experiment for parabolic flight was a downscaled process of Envisat capturing. The prepacked net was launched towards the satellite model, it expanded, hit the model and wrapped around it. The whole process was recorded with 2 fast stereographic camera sets for full 3D trajectory reconstruction. The trajectories were used to compare net dynamics to respective simulations and then to validate the simulation tool. The experiments were performed on board of a Falcon-20 aircraft, operated by National Research Council in Ottawa, Canada. Validation results show that model reflects phenomenon physics accurately enough, so it may be used for scenario evaluation and mission design purposes. The functionalities of the simulator are described in detail in the paper, as well as its underlying model, sample cases and methodology behind validation. Results are presented and typical use cases are discussed showing that the software may be used to design throw nets for space debris capturing, but also to simulate deorbitation process, chaser control system or general interactions between rigid and elastic bodies – all in convenient and efficient way. The presented work was led by SKA Polska under the ESA contract, within the CleanSpace initiative. •A simulator was developed for space debris capturing with deplayable nets.•It simulates dynamics of systems made of tethers, cords, ropes, etc. and rigid bodies.•Cosserat Rods theory is used allowing to simulate stretching, bending and torsion.•Software was validated with down-scaled experiment in parabolic flight.