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检索条件"主题词=iterative Algorithm"
1762 条 记 录,以下是1731-1740 订阅
排序:
PRINCIPAL COORDINATE REALIZATION OF STATE ESTIMATION AND ITS APPLICATION TO ORDER REDUCTION
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1988年 第3期11卷 286-288页
作者: MIYAZAWA, Y DOWELL, EH DUKE UNIV SCH ENGNDURHAMNC 27706
A set of singular values is proposed for use as a plant dynamics-modeling quantitative index which expresses estimation accuracy in terms of the state components. Since the singular values show not only estimation qua... 详细信息
来源: 评论
CALCULATION OF GEODETIC COORDINATES FROM EARTH-CENTERED, EARTH-FIXED COORDINATES
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1988年 第2期11卷 188-190页
作者: OLSON, DK U.S. Navy Pacific Missile Test Center Point Mugu CA
A simple refinement is proposed for Gersten's (1961) method for the conversion of earth-centered, earth-fixed (ECEF) coordinates to geodetic coordinates. The refinement, which involves conversion of the appropriat... 详细信息
来源: 评论
ONE-SIDED CONFIDENCE-INTERVALS FOR THE POSITIVE LINEAR COMBINATION OF 2 VARIANCES
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COMMUNICATIONS IN STATISTICS-SIMULATION AND COMPUTATION 1988年 第1期17卷 283-292页
作者: WANG, CM Computer Science Department General Motor Research Laboratories Warren Michigan 48090 United States
In this article the existing methods for determining the approximate onesided confidence intervals on the positive linear combinations of two variances are examined. In addition, an iterative algorithm which can be us... 详细信息
来源: 评论
algorithm TO GENERATE GEODETIC COORDINATES FROM EARTH-CENTERED EARTH-FIXED COORDINATES
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1988年 第3期11卷 281-283页
作者: NAUTIYAL, A Defence Research and Development Laboratory Hyderabad India
The iterative algorithm presented for the transformation of earth-centered, earth-fixed coordinates into geodetic coordinates is free from any singularity, has a uniformly good rate of convergence from the equator to ... 详细信息
来源: 评论
A RESOLUTION METHOD FOR RICCATI DIFFERENTIAL-SYSTEMS COUPLED IN THEIR QUADRATIC TERMS
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SIAM JOURNAL ON MATHEMATICAL ANALYSIS 1988年 第6期19卷 1425-1430页
作者: JODAR, L ABOUKANDIL, H ECOLE SUPER ELECT SIGNAUX & SYST LAB CNRS F-91190 GIF SUR YVETTE FRANCE
By means of algebraic transformations a Riccati differential matrix system coupled in its quadratic terms is reduced to another one for which the successive approximation method is available. An iterative algorithm fo... 详细信息
来源: 评论
AN iterative algorithm BETWEEN STREAM FUNCTION AND DENSITY FOR TRANSONIC CASCADE FLOW
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JOURNAL OF PROPULSION AND POWER 1986年 第3期2卷 259-265页
作者: WANG, BG Chinese Academy of Sciences Institute of Engineering Thermophysics Beijing People's Republic of China
A set of Wu 's equations governing the fluid flow along a given Si stream surface is solved by the use of artificialcompressibility and a new iterative algorithm between the two variables stream function ^ and den... 详细信息
来源: 评论
iterative algorithmS FOR THE LINEAR COMPLEMENTARITY-PROBLEM
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INTERNATIONAL JOURNAL OF COMPUTER MATHEMATICS 1986年 第3-4期19卷 273-297页
作者: KAPPEL, NW WATSON, LT VIRGINIA POLYTECH INST & STATE UNIV DEPT COMP SCIBLACKSBURGVA 24061
Direct complementary pivot algorithms for the linear complementarity problem withP-matrices are known to have exponential computational complexity. The analog of Gauss-Seidel and SOR iteration for linear complementari... 详细信息
来源: 评论
COMPARISON OF ANGULAR AND METRIC GUIDANCE LAWS FOR TACTICAL MISSILES
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1986年 第4期9卷 505-507页
作者: DURIEUX, JL Cabinet d'Etudes Techniques d'Automatisation Angouleme France
An angular guidance law for tactical missiles optimized by the adjoint technique is compared with a metric law for such missiles comprising an estimator connected to a terminal controller forcing the estimated miss di... 详细信息
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A SIMPLE algorithm FOR THE SELECTION OF TERMINAL PENALTY WEIGHTING MATRICES
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1986年 第4期9卷 503-505页
作者: CHUN, HM TURNER, JD CAMBRIDGE RES CONTROL THEORY DYNAM GRPCAMBRIDGEMA
A simple iterative algorithm for selecting terminal penalty weighting matrices for linear-quadratic control problems is presented. The algorithm selects a weighting matrix which yields acceptable system performance, w... 详细信息
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AIRCRAFT CONTROL DESIGN USING IMPROVED TIME-DOMAIN STABILITY ROBUSTNESS BOUNDS
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JOURNAL OF GUIDANCE CONTROL AND DYNAMICS 1986年 第6期9卷 710-714页
作者: YEDAVALLI, RK LIANG, Z STEVENS INST TECHNOL DEPT MECH ENGNHOBOKENNJ 07030
This paper addresses the issue of "conservatism" in the time-domain stability robustness bounds obtained by the Lyapunov approach. A state transformation is employed to improve the upper bounds on the linear... 详细信息
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