4 results found Select / deselect all results (all pages, 4 total) Numerical Simulations for Spacecraft Catastrophic Disruption Analysis At present, the largest part of the catalogued space debris population consists of fragments originating from accidental explosions of spacecraft and upper stages, but it is expected that hypervelocity collisions involving large objects could become the primary source of new debris in the mid-term future. In this context, understanding the physical processes involved in spacecraft collisions is crucial, because these big impacts are one of the key drivers of the long-term evolution of the amount of space debris. Italy Discovery 15/716-a CISAS 2016 - 2019 Numerical Simulations for Spacecraft Catastrophic Disruption Analysis Numerical Simulations for Spacecraft Catastrophic Disruption Analysis While the vast majority of space debris still stems from explosion events of satellites and rocket upper stages, current forecasts state that collisions, such as those between the Cosmos 2251 and Iridium 33 satellites in 2009, will play a dominant role in the mid-term future when a critical spatial density of satellites has been reached. In order to assess the risks emanating from space debris, a deeper understanding of the formation and residence time of breakup debris in orbit is essential for operational activities. Germany Discovery 15/716-b Fraunhofer Gesellschaft 2016 - 2018 Numerical Simulations for Spacecraft Catastrophic Disruption Analysis Investigation of Active Detumbling Solutions for Debris Removal The main objective of this study 'DETUMBLING – Investigation of Active Detumbling Solutions for Debris Removal' was to propose and investigate a contact-based de-tumbling strategy using a robotic arm. Realistic models were developed for the chaser with robotic-arm, target and composite systems. Specific GNC strategies were developed for the different phases of the mission: robotic-arm deployment synchronisation with the target de-tumbling the composite. Spain Discovery 13-054 GMV 2014 - 2017 Investigation of Active Detumbling Solutions for Debris Removal High performance avionics solution for advanced and complex GNC systems (HIPNOS) The objective of this document is the presentation of the final synthesis of the activity “HIPNOS”, Development of a representative HW/SW solution for a high-performance processing platform for Active Debris Removal missions. Implement COTS-based solution as Demonstration of the activity. HIPNOS includes trade-off study of processing technologies, processing space-grade and COTS devices, processing architectures, trade-off for computer vision algorithms, and demonstrator of the selected solution. The scope and objectives of the activity are: Spain Discovery 13-121 GMV 2016 - 2017 High performance avionics solution for advanced and complex GNC systems (HIPNOS) Filter by Programme Discovery (4) Filter by Start Year 2016 (3) 2014 (1) Filter by End Year 2017 (2) 2018 (1) 2019 (1) Filter by Keywords ADR (2) AOCS (1) Avionics (1) Catastrophic collisions (1) Dynamics (1) GNC (1) High velocity (1) Hypervelocity (1) Impact (1) Model (1) (-) Simulation (4) (-) Space debris (4) Filter by Contractor GMV (2) CISAS (1) Fraunhofer Gesellschaft (1) Filter by Country Spain (2) Germany (1) Italy (1) Filter by Application Domain Generic Technologies (2) Space Safety (2) Filter by Technology Domain 11 - Space Debris (3) 4 - Space Systems Environments and Effects (1) Filter by Competence Domain 10-Astrodynamics, Space Debris and Space Environment (3) Filter by Activity Status Closed (3)