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About us Spacecraft structuresTerms of ReferenceDuties of the Structures sectionTechnology areas Antenna structuresComposite Materials structuresFracture control / Damage toleranceInflatable structures for space applicationsMeteoroid and debris shieldingStructural verification of payloads and system hardware for human rated vehiclesStructural design and analysis Configuration studiesStructural AnalysisLauncher-Spacecraft Coupled Loads AnalysisFluid Structure InteractionVibro-Accoustic AnalysisProject support Project support activitiesServices EventsContact us
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The Mechanisms Section performs detailed analyses involving flexible bodies with time-varying characteristics and control algorithms. The software programs used are DCAP (based on a ‘fast’, ‘effective’ and ‘symbolic’ formulation), Adams, SIMPACK and SAMCEF Mecano. Several Mechanisms Dynamics Activities have been performed in support of numerous projects:
Mechanisms:
- design and analyse mechanisms systems
- assess parametric design solutions and to optimise the performances of structures and mechanisms
- predict the static, kinematics and dynamic behaviour of mechanical systems
- animate the motion of dynamic, solid models
- simulate control loops incorporating mechanical parts, e.g. mechanisms active structures
- perform conceptual design studies and correlate test and analysis data
- investigate the performance and possible malfunction of mechanical systems, including in-orbit
- modelling complex devices and mechanisms control design
- coupled system frequencies and time responses
Spacecrafts:
- modelling unconventional S/C dynamics, including orbital environment disturbances
- control laws, including sensors and actuation dynamics
- coupled system frequencies and time responses
- docking phase analyses
Launch Vehicles:
- non-linear time dynamic simulations for flexible bodies with time varying characteristics
- atmospheric environment including external disturbance
- launch vehicle flight dynamics-control interaction (directly imported into Matlab)
- frequency domain analysis
- multiple nozzles dynamics capabilities
- local analyses (gust response, lift off, multi-payload separations)
- collision avoidance
- data recovery procedure
Last update: 19 January 2011 | |
| ![](../../global_imgs/spacer.gif) | Conference papers Variable mass and Simulink I/F (pdf)Data Recovery Procedure (pdf)Related article DCAP Thales Alenia Space ItalyRelated Links SAMCEF Mecano SamtechAdams MSC.SoftwareSIMPACK SIMPACK AGESA Workshop 1st ESA Workshop on Multibody Dynamics for Space ApplicationsPresentation MAST overview (pdf)More information Multibody & Advanced Simulation TeamBearing Life AssessmentElectromagnetics, ElectrostaticsFeasibilities studies (CDF)ISS payloadsLauncher Flight Dynamics SimulatorMechanism Component AnalysisOn-Ground Test and In-Flight Telemetry Data Analysis
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