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- W2335624417 abstract "One of the many challenging domains of aerospace analysis is related to multi-body dynamics or kinematics. To accurately simulate spacecraft and aircraft performance, such as landing gears, solar panel deployment or other deployment mechanisms, one needs to include mechanisms, flexible bodies, nonlinear effects related to the joints like friction and contact, nonlinear geometry effects, external loads such as gravity and air resistance during ground tests, and control systems that drive the deployments. Traditionally these types of problems are not solved in a single simulation, but rather broken up into several different simulations and very often assumptions are made and large margins of safety are applied. Recent enhancements to commercial finite element analysis (FEA) software codes enable this complete problem to be solved as a coupled simulation. This paper examines the methodology and capability of solving aerospace multi-body dynamics (MBD) problems using Abaqus." @default.
- W2335624417 created "2016-06-24" @default.
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- W2335624417 date "2011-04-04" @default.
- W2335624417 modified "2023-09-25" @default.
- W2335624417 title "Advanced Multi-Body Dynamics: Fully Coupled Kinematics with Nonlinear FEA" @default.
- W2335624417 doi "https://doi.org/10.2514/6.2011-1872" @default.
- W2335624417 hasPublicationYear "2011" @default.
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