LIMIT-CYCLE ANALYSIS OF HYDROELECTRIC SYSTEMS

被引：3
|
作者：
PANTALONE, DK
PIEGZA, DM
机构：
来源：
IEEE TRANSACTIONS ON POWER APPARATUS AND SYSTEMS | 1981年 / 100卷 / 02期
关键词：
D O I：
10.1109/TPAS.1981.316919
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
引用
收藏
页码：629 / 638
页数：10
相关论文
共 50 条
  • [31] ON VERIFICATION OF LIMIT-CYCLE STABILITY IN AUTONOMOUS NONLINEAR-SYSTEMS
    QIU, SS
    FILANOVSKY, IM
    IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS, 1988, 35 (08): : 1062 - 1064
  • [32] Reduced order modeling of limit-cycle oscillation for aeroelastic systems
    Beran, PS
    Lucia, DJ
    Pettit, CL
    PROCEEDINGS OF THE 5TH INTERNATIONAL SYMPOSIUM ON FLUID STRUCTURE INTERACTION, AEROELASTICITY, FLOW INDUCED VIBRATION AND NOISE, PTS A AND B, 2002, : 13 - 24
  • [33] ON THE LIMIT-CYCLE DISTRIBUTION OVER 2 NESTS IN QUADRATIC SYSTEMS
    HUANG, XH
    REYN, JW
    BULLETIN OF THE AUSTRALIAN MATHEMATICAL SOCIETY, 1995, 52 (03) : 461 - 474
  • [34] SIMPLE CHEMICAL-REACTION SYSTEMS WITH LIMIT-CYCLE BEHAVIOR
    SCHNAKENBERG, J
    JOURNAL OF THEORETICAL BIOLOGY, 1979, 81 (03) : 389 - 400
  • [35] LIMIT-CYCLE STABILITY OF SYSTEMS CONTAINING A PULSE RATIO MODULATOR
    ALLDRIDGE, WJ
    AERONAUTICAL JOURNAL, 1978, 82 (814): : 440 - 445
  • [36] LIMIT-CYCLE PHENOMENA IN NONLINEAR TIME-DELAY SYSTEMS
    BARKHAM, PGD
    SOUDACK, AC
    INTERNATIONAL JOURNAL OF CONTROL, 1978, 27 (03) : 407 - 420
  • [37] Nonlinear System Identification of Systems with Periodic Limit-Cycle Response
    M. Thothadri
    F. C. Moon
    Nonlinear Dynamics, 2005, 39 : 63 - 77
  • [38] Limit-cycle phase in driven-dissipative spin systems
    Chan, Ching-Kit
    Lee, Tony E.
    Gopalakrishnan, Sarang
    PHYSICAL REVIEW A, 2015, 91 (05):
  • [39] Nonlinear system identification of systems with periodic limit-cycle response
    Thothadri, M
    Moon, FC
    NONLINEAR DYNAMICS, 2005, 39 (1-2) : 63 - 77
  • [40] Numerical analysis of store-induced limit-cycle oscillation
    Beran, PS
    Khot, NS
    Eastep, FE
    Snyder, RD
    Zweber, JV
    JOURNAL OF AIRCRAFT, 2004, 41 (06): : 1315 - 1326
12345