DESIGN OF ADAPTIVE DIGITAL MODEL-FOLLOWING FLIGHT-MODE CONTROL-SYSTEMS FOR HIGH-PERFORMANCE AIRCRAFT

被引:0
|
作者
PORTER, B
OTHMAN, MZ
机构
来源
AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS | 1989年
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:593 / 601
页数:9
相关论文
共 50 条
  • [1] DESIGN OF DIGITAL FLIGHT-MODE CONTROL-SYSTEMS FOR HELICOPTERS WITH NON-LINEAR ACTUATORS
    PORTER, B
    AERONAUTICAL JOURNAL, 1985, 89 (886): : 213 - 218
  • [2] DESIGN OF GENERAL MODEL-FOLLOWING CONTROL-SYSTEMS
    SHAKED, U
    INTERNATIONAL JOURNAL OF CONTROL, 1977, 25 (01) : 57 - 79
  • [3] Model-Following Sliding Mode Controller Design for Flight Control Systems with Wind Disturbances
    Yang Zhi-jun
    Qi Xiao-hui
    Shan Gan-lin
    ICIEA: 2009 4TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, VOLS 1-6, 2009, : 282 - 286
  • [4] MULTIVARIABLE VARIABLE-STRUCTURE ADAPTIVE MODEL-FOLLOWING CONTROL-SYSTEMS
    ZINOBER, ASI
    ELGHEZAWI, OME
    BILLINGS, SA
    IEE PROCEEDINGS-D CONTROL THEORY AND APPLICATIONS, 1982, 129 (01): : 6 - 12
  • [5] DESIGN OF MULTIVARIABLE ADAPTIVE MODEL FOLLOWING CONTROL-SYSTEMS
    LANDAU, ID
    COURTIOL, B
    AUTOMATICA, 1974, 10 (05) : 483 - 494
  • [6] Pitch autopilot design using model-following adaptive sliding mode control
    Choe, DG
    Kim, JH
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2002, 25 (04) : 826 - 829
  • [7] Fault Tolerant Flight Control Law Design with a Model-Following Sliding Mode Controller
    Yang Zhi-jun
    Qi Xiao-hui
    Shan Gan-lin
    2009 INTERNATIONAL CONFERENCE ON MEASURING TECHNOLOGY AND MECHATRONICS AUTOMATION, VOL I, 2009, : 665 - 668
  • [8] Flight data reduction methodology for performance evaluation and comparison of model-following adaptive control laws
    Perhinschi, M. G.
    Napolitano, M. R.
    AERONAUTICAL JOURNAL, 2007, 111 (1126): : 807 - 814
  • [9] HIGH-PERFORMANCE AIRCRAFT AND ADAPTIVE CONTROL
    不详
    CONTROL, 1967, 11 (105): : 110 - &
  • [10] DIGITAL CONTROL OF HIGH-PERFORMANCE AIRCRAFT USING ADAPTIVE ESTIMATION TECHNIQUES
    VANLANDINGHAM, HF
    MOOSE, RL
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1977, 13 (02) : 112 - 119