EQUIVALENT LINE TRANSFORMATIONS IN ELECTRIC NETWORK DESIGN FOR MINIMAL WEIGHT.

被引：0
|
作者：
Shchedrin, O.P.
机构：
来源：
Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika) | 1986年 / 29卷 / 03期
关键词：
ELECTRIC POWER TRANSMISSION - Network Calculations;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The solution of optimization problems in flight vehicle electrical systems design - location of the switching devices (SD) and selection of the cross-sections of the connecting wires under conditions of large dimensionality - involves significant procedural and computational difficulties. The objective of the present work is the analysis of two forms of equivalent transformations of optimal radial branched (tree-like) systems: convolution and splitting, simplifying the solution of the subject problems.
引用
收藏
页码：117 / 121
相关论文
共 50 条
  • [1] FRACTIONATION OF SODIUM SULFONATES ACCORDING TO EQUIVALENT WEIGHT.
    Kachmar, O.S.
    Gud, L.N.
    Bodan, A.N.
    Chemistry and Technology of Fuels and Oils, 1984, 20 (08) : 408 - 411
  • [2] EQUIVALENT FEED-LINE TRANSFORMATIONS DURING ELECTRICAL NETWORK DESIGN USING MASS CRITERION
    SHCHEDRIN, OP
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1986, 3 : 87 - 90
  • [3] OFFSHORE FLARE DESIGN TO SAVE WEIGHT.
    Barnwell, Julian
    Marshall, B.K.
    Energy progress, 1985, 5 (01): : 33 - 39
  • [4] On the discrimination of minimal differences in weight. III. The role of frequency
    Holway, AH
    Smith, JE
    Zigler, MJ
    JOURNAL OF EXPERIMENTAL PSYCHOLOGY, 1937, 21 : 423 - 432
  • [5] APPLICATION OF N-TERMINAL NETWORK EQUIVALENT TRANSFORMATIONS TO THE PROBLEM OF EQUIVALENT-CIRCUIT DESIGN
    ZINCHENKO, LA
    ELECTRICAL TECHNOLOGY, 1993, (01): : 131 - 138
  • [6] DESIGN METHOD FOR MEANDER-LINE NETWORKS USING EQUIVALENT CIRCUIT TRANSFORMATIONS
    SATO, R
    IEEE TRANSACTIONS ON MICROWAVE THEORY AND TECHNIQUES, 1971, MT19 (05) : 431 - &
  • [7] CANONIC LC EQUIVALENT NETWORK TRANSFORMATIONS
    YARLAGADDA, R
    TAKAD, Y
    PROCEEDINGS OF THE INSTITUTION OF ELECTRICAL ENGINEERS-LONDON, 1966, 113 (06): : 982 - +
  • [8] STEP BY STEP DESIGN OF AN AIRPLANE WING FOR MINIMUM WEIGHT.
    Patel, T.S.
    Trabelsi, S.B.
    Al-Colfat, A.A.
    Modelling, simulation & control. B, 1987, 11 (02): : 55 - 64
  • [9] DESIGN OF A TWO-SPAR WING OF AN AIRCRAFT FOR MINIMUM WEIGHT.
    Patel, T.S.
    Abdussalam, S.R.
    Modelling, simulation & control. B, 1984, 1 (03): : 17 - 28
  • [10] MINIMAL WEIGHT DESIGN FOR CONICAL SHELLS
    REISS, R
    JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1974, 41 (03): : 599 - 603
12345