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INERTIAL ALGORITHMS FOR THE STATIONARY NAVIER-STOKES EQUATIONS
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作者 侯延仁 R.M.M.Mattheij 《Acta Mathematica Scientia》 SCIE CSCD 2003年第2期219-238,共20页
Several kind of new numerical schemes for the stationary Navier-Stokes equations based on the virtue of Inertial Manifold and Approximate Inertial Manifold, which we call them inertial algorithms in this paper, togeth... Several kind of new numerical schemes for the stationary Navier-Stokes equations based on the virtue of Inertial Manifold and Approximate Inertial Manifold, which we call them inertial algorithms in this paper, together with their error estimations are presented. All these algorithms are constructed under an uniform frame, that is to construct some kind of new projections for the Sobolev space in which the true solution is sought. It is shown that the proposed inertial algorithms can greatly improve the convergence rate of the standard Galerkin approximate solution with lower computing effort. And some numerical examples are also given to verify results of this paper. 展开更多
关键词 Navier-Stokes equations error estimation inertial algorithms
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Pseudo-linear inertial navigation algorithm 被引量:3
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作者 Habib GHANBARPOURASL 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2021年第2期191-200,共10页
A new method is illustrated for processing the output of a set of triad orthogonal rate gyros and accelerometers to reconstruct vehicle navigation parameters(attitude, velocity, and position). The paper introduces two... A new method is illustrated for processing the output of a set of triad orthogonal rate gyros and accelerometers to reconstruct vehicle navigation parameters(attitude, velocity, and position). The paper introduces two vectors with dimensions 4×1 as velocity and position quaternions.The navigation equations for strapdown systems are nonlinear but after using these parameters, the navigation equations are converted into a pseudo-linear system. The new set of navigation equations has an analytical solution and the state transition matrix is used to solve the linear timevarying differential equations through time series. The navigation parameters are updated using the new formulation for strapdown navigation equations. Finally, the quaternions of velocity and position are converted into the original position and velocity vectors. The combination of the coning motion and a translational oscillatory trajectory is used to evaluate the accuracy of the proposed algorithm. The simulations show significant improvement in the accuracy of the inertial navigation system, which is achieved through the mentioned algorithm. 展开更多
关键词 inertial navigation algorithm Integrating algorithm Position quaternion Pseudo-linear inertial navigation equation QUATERNIONS Velocity quaternion
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