We regard the real symplectic group Sp(2n,R)\documentclass[12pt] as a constraint submanifold of the 2nx2n\documentclass[12pt] real matrices M2n(R)\documentclass[12pt] endowed with the Euclidean (Frobenius) metric, res...
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We regard the real symplectic group Sp(2n,R)\documentclass[12pt] as a constraint submanifold of the 2nx2n\documentclass[12pt] real matrices M2n(R)\documentclass[12pt] endowed with the Euclidean (Frobenius) metric, respectively as a submanifold of the general linear group Gl(2n,R)\documentclass[12pt] endowed with the (left) invariant metric. For a cost function that defines an optimization problem on the real symplectic group we give a necessary and sufficient condition for critical points and we apply this condition to the particular case of a least square cost function. In order to characterize the critical points we give a formula for the Hessian of a cost function defined on the real symplectic group, with respect to both considered metrics. For a generalized Brockett cost function we present a necessary condition and a sufficient condition for local minimum. We construct a retraction map that allows us to detail the steepestdescent and embedded Newton algorithms for solving an optimization problem on the real symplectic group.
High-resolution transmission electron microscopy (HRTEM) images can capture the atomic-resolution details of the dynamically changing structure of nanomaterials. Here, we propose a new scheme and an improved reconstru...
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High-resolution transmission electron microscopy (HRTEM) images can capture the atomic-resolution details of the dynamically changing structure of nanomaterials. Here, we propose a new scheme and an improved reconstruction algorithm to reconstruct the exit wave function for each image in a focal series of HRTEM images to reveal structural changes. In this scheme, the wave reconstructed from the focal series of images is treated as the initial wave in the reconstruction process for each HRTEM image. Additionally, to suppress noise at the frequencies where the signal is weak due to the modulation of the lens transfer function, a weight factor is introduced in the improved reconstruction algorithm. The advantages of the new scheme and algorithms are validated by using the HRTEM images of a natural specimen and a single-layer molybdenum disulphide. This algorithm enables image resolution enhancement and lens aberration removal, while potentially allowing the visualisation of the structural evolution of nanostructures.
This paper proposes a Novel least mean square algorithm using First order Al-Alaoui *** performance of the proposed algorithm is compared with existing algorithms by taking an example. The results prove the efficacy o...
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This paper proposes a Novel least mean square algorithm using First order Al-Alaoui *** performance of the proposed algorithm is compared with existing algorithms by taking an example. The results prove the efficacy of the proposed algorithm.
We implement space mapping technique for the first time to optimize geometry of a glass tube during its production process. The strategy is to align the optimizer of the coarse model (isothermal tube drawing) with the...
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We implement space mapping technique for the first time to optimize geometry of a glass tube during its production process. The strategy is to align the optimizer of the coarse model (isothermal tube drawing) with the fine model (nonisothermal tube drawing) through space mapping technique in order to find an optimal solution of a control problem. Adjoint variable approach is used to find optimizer of the coarse model. Numerical results obtained through aggressive space mapping (ASM) algorithm are presented and discussed.
We show that the steepest descent algorithm in connection with wiggly energies yields minimizing sequences that converge to a global minimum of the associated non-quasiconvex variational integrals. We introduce a mult...
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We show that the steepest descent algorithm in connection with wiggly energies yields minimizing sequences that converge to a global minimum of the associated non-quasiconvex variational integrals. We introduce a multi-level infinite dimensional variant of the steepest descent algorithm designed to compute complex microstructures by forming nonsmooth minimizers from the smooth initial guesses. We apply this multilevel method to the minimization of the variational problems associated with martensitic branching.
We consider a class of alloys and ceramics with equilibria described by non-attainable infima of non-quasiconvex variational integrals. Such situations frequently arise when atomic lattice structure plays an important...
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We consider a class of alloys and ceramics with equilibria described by non-attainable infima of non-quasiconvex variational integrals. Such situations frequently arise when atomic lattice structure plays an important role at the mesoscopic continuum level. We prove that standard variational approaches associated with gradient based relaxation of non-quasiconvex integrals in Banach or Hilbert spaces are not capable of generating relaxing sequences for problems with non-attainable structure. We introduce a variational principle suitable for the computational purposes of approaching non-attainable infima of variational integrals. We demonstrate that this principle is suitable for direct calculations of the Young Measures on a computational example in one dimension. The new variational principle provides the possibility to approximate crystalline microstructures using a Fokker-Planck equation at the meso-scale. We provide an example of such a construction. (C) 2003 Elsevier B.V. All rights reserved.
We define a hereditary system on a finite set U as a partition of the family 2(U) of all subsets of U into disjoint families A and D satisfying (A is an element of V, A' subset of or equal to A) double right arrow...
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We define a hereditary system on a finite set U as a partition of the family 2(U) of all subsets of U into disjoint families A and D satisfying (A is an element of V, A' subset of or equal to A) double right arrow A' is an element of A and (D is an element of D, D subset of or equal to D') = double right arrow D' is an element of D, respectively. The members of A are called independent sets, the sets D is an element of D are called dependent. We consider two important special cases of hereditary systems, matroids and comatroids, and study the structure of these objects. Two general combinatorial optimization problems on a hereditary system, the maximum independent set problem max{f (X): X is an element of A} and the minimum dependent set problem min{f(X): X is an element of D}, are considered. Jenkyns, Korte and Hausmann obtained a performance guarantee of the greedy heuristic ('best in') for the maximum independent set problem. We present a greedy-type approximation algorithm for solving the minimum dependent set problem, the steepestdescent heuristic ('worst out'), study interconnections between the above-mentioned problems and derive performance guarantees of the steepest descent algorithm. Finally, we apply our results to obtain performance guarantees of the steepest descent algorithm for some known special combinatorial minimization problems. (C) 2003 Elsevier B.V. All rights reserved.
According to the modern control and optimal estimation theory, a mathematical model of the pilot attention resource allocation is developed. This model analyzes the inherent characteristics of pilot input and output l...
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ISBN:
(纸本)9781479920303
According to the modern control and optimal estimation theory, a mathematical model of the pilot attention resource allocation is developed. This model analyzes the inherent characteristics of pilot input and output links in the pilot-vehicle closed-loop system, and the optimal control model of pilot is established by simplification and mathematical modeling. The control task chosen in this paper concerns the longitudinal motion of a hovering aircraft. To solve the pilot optimal attention allocation problem in the instrument-monitoring task of the pilot-vehicle closed-loop system an objective function is set up based on flight control system state equation. In the process of solving optimization problem, the constrained optimization problem is converted into an unconstrained problem, and is solved effectively with the method of steepest descent algorithm in the MATLAB.
This paper presents a novel procedure to calibrate the strap-down 3-axis MEMS accelerometers for UAV navigat-ion. Firstly, we establish an explicit calibration model with the measurement values of accelerometers, wher...
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ISBN:
(纸本)9783037853122
This paper presents a novel procedure to calibrate the strap-down 3-axis MEMS accelerometers for UAV navigat-ion. Firstly, we establish an explicit calibration model with the measurement values of accelerometers, where the calibration is realized via geometric transformations. Secondly, the transfor-mation parameters are calculated through particle swarm optimization (PSO). For the problem of slower convergence rates near the global optimum, the classical PSO algorithm is improved. Based on the numerical optimization idea, the steepestdescent method is introduced to PSO. The parameters are searched in the rough by adopting PSO and the precision ones are found by using steepestdescent method. Then, the optimal transformation is achieved by the minimum distance function based on this improved PSO(IPSO) algorithm. Finally, the calibration procedure is tested by comparing the attitude produced by the 3-axis accelerometers with that measured by a turntable. The results show that the IPSO algorithm can significantly improve the performance of the classical PSO algorithm, and the maximum attitude error is reduced to 6% of that before calibration. In addition, the proposed procedure does not rely on prior knowledge of the accelerometers and any equipment. So, it is suitable for calibration in field. Such a method is especially useful in UAV applications.
A Novel Least Mean Square(LMS) algorithm using First order Al-Alaoui differentiator is proposed. The condition for stability is also derived. The performance of the novel technique is compared with existing algorithms...
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ISBN:
(纸本)9781509006298
A Novel Least Mean Square(LMS) algorithm using First order Al-Alaoui differentiator is proposed. The condition for stability is also derived. The performance of the novel technique is compared with existing algorithms by taking an example. The results prove the efficacy of the proposed algorithm.
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