VSTOL FIRST FLIGHT OF AN H-INFINITY CONTROL LAW

被引:12
|
作者
HYDE, RA
GLOVER, K
SHANKS, GT
机构
[1] DEF RES AGCY,BEDFORD,ENGLAND
[2] UNIV CAMBRIDGE,DEPT ENGN,CAMBRIDGE,ENGLAND
来源
关键词
D O I
10.1049/cce:19950107
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
An H-infinity control law has been successfully flight tested on the DRA Bedford Harrier. This and subsequent flight tests demonstrated the practicality and power of H-infinity as a design tool for systems with multiple inputs and outputs. The technique has potential both to reduce design time, and to improve robustness and performance for such systems. This article discusses the development of the control law and some of the challenging implementation issues which had to be addressed in order to bridge the gap between theory and practice.
引用
收藏
页码:11 / 16
页数:6
相关论文
共 50 条
  • [1] VSTOL first flight of an H∞ control law
    [J]. Comput Control Eng J, 1 (11-16):
  • [2] COMPARISON OF CHARACTERISTIC LOCUS AND H-INFINITY METHODS IN VSTOL FLIGHT CONTROL-SYSTEM DESIGN
    WILLIAMS, SJ
    SMITH, PR
    [J]. AIAA GUIDANCE, NAVIGATION AND CONTROL CONFERENCE, PTS 1 AND 2: A COLLECTION OF TECHNICAL PAPERS, 1989, : 565 - 575
  • [3] Nonlinear H-infinity flight control
    Yang, CD
    Kung, CC
    [J]. PROCEEDINGS OF THE 1997 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 1997, : 140 - 144
  • [4] THE APPLICATION OF SCHEDULED H-INFINITY CONTROLLERS TO A VSTOL AIRCRAFT
    HYDE, RA
    GLOVER, K
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1993, 38 (07) : 1021 - 1039
  • [5] H-INFINITY OBSERVATIONS WEIGHTED CONTROL LAW
    GRIMBLE, MJ
    [J]. JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 1990, 112 (03): : 337 - 348
  • [6] H-INFINITY OBSERVATIONS WEIGHTED CONTROL LAW
    GRIMBLE, MJ
    [J]. PROCEEDINGS OF THE 1989 AMERICAN CONTROL CONFERENCE, VOLS 1-3, 1989, : 759 - 764
  • [7] H-INFINITY MULTIVARIABLE-CONTROL-LAW SYNTHESIS
    GRIMBLE, MJ
    [J]. IEE PROCEEDINGS-D CONTROL THEORY AND APPLICATIONS, 1993, 140 (05): : 353 - 363
  • [8] H-INFINITY HELICOPTER FLIGHT CONTROL LAW DESIGN WITH AND WITHOUT ROTOR STATE-FEEDBACK
    TAKAHASHI, MD
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (06) : 1245 - 1251
  • [9] H-INFINITY CONTROL WITH TRANSIENTS
    KHARGONEKAR, PP
    NAGPAL, KM
    POOLLA, KR
    [J]. SIAM JOURNAL ON CONTROL AND OPTIMIZATION, 1991, 29 (06) : 1373 - 1393
  • [10] Tracking performance analysis of flight control system based on H-infinity theory
    Dong, Shuai
    Wang, Zhisheng
    Wang, Yongji
    Liu, Lei
    Ou, Liuli
    [J]. INTERNATIONAL JOURNAL OF MODELLING IDENTIFICATION AND CONTROL, 2013, 19 (03) : 290 - 298