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The main purpose of this paper is to present a pretension design method for space deployable mesh reflectors under multi-uncertainty.
The explicit finite element method for transient dynamics of linear elasticity is formulated by using Galerkin method for space and the central difference method for time.
Our approach hinges on the following essential features: shape differential calculus, a semi-implicit time discretization and a finite element method for space discretization.
Then combining with the anti-optimization strategy, a pretension design method for space deployable mesh reflectors considering multi-uncertainty is proposed to minimize the influence from the uncertainties.
This paper presents a novel obstacle avoidance constraint and a mixed integer predictive control (MIPC) method for space robots avoiding obstacles and satisfying physical limits during performing tasks.
Our formulation is based on a mixed finite element method for space discretization and a new second-order accurate time integration algorithm.
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An automatic abstraction method for state space is proposed by using the Gauss basis function and inner evaluation indexes to speed up the learning process.
In this paper, a new design method for space-time trellis codes in MB-OFDM systems with correlated Rayleigh fading channels is introduced.
Aspiration of dead space (ASPIDS), a known method for dead space reduction, comprises two mechanisms activated during late expiration: aspiration of gas from the tip of the tracheal tube and gas injection through the inspiratory line - circuit flushing.
Numerical methods for space-fractional diffusion equations often generate dense or even full stiffness matrices.
Because of the non-local property of fractional differential operators, numerical methods for space-fractional diffusion equations generate dense or even full coefficient matrices with complicated structures.
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