Near optimal state feedback design for singularly perturbed systems by unified approach with an aircraft application

被引：0
|
作者：
Shim, KH [1 ]
Sawan, ME [1 ]
机构：
[1] Wichita State Univ, Dept Elect & Comp Engn, Wichita, KS 67260 USA
来源：
PROCEEDINGS OF THE 37TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4 | 1998年
关键词：
delta operator q(shift) operator; finite word-length characteristics; two-time-scale analysis; near-optimal control;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A state feedback design in two-time-scale systems is presented by a unified approach, which adopts delta (delta) operators. The discrete system given is converted to a unified system and is decomposed into the slow and fast subsystems. Then, we formulate the necessary equations and algorithm to obtain the de-coupled and exact solutions. Here, an aircraft implementation is made. And the results of both discrete and unified solutions are shown and compared.
引用
收藏
页码：3177 / 3182
页数：6
相关论文
共 50 条
  • [1] Near optimal state feedback design for singularly perturbed systems by unified approach with an aircraft application
    Shim, Kyu-Hong
    Sawan, M.Edwin
    Proceedings of the IEEE Conference on Decision and Control, 1998, 3 : 3177 - 3182
  • [2] Near-optimal state feedback design for singularly perturbed systems by unified approach
    Shim, KH
    Sawan, ME
    INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2002, 33 (03) : 197 - 212
  • [3] State feedback design for singularly perturbed system using unified approach
    Chenxiao Cai
    Yun Zou
    Duanjin Zhang
    Journal of Control Theory and Applications, 2004, 2 (3): : 276 - 280
  • [4] State feedback design for singularly perturbed system using unified approach
    Chenxiao CAI
    College of Information Engineering
    Journal of Control Theory and Applications, 2004, (03) : 276 - 280
  • [5] Robust stability of singularly perturbed state feedback systems using unified approach
    Singh, H
    Brown, RH
    Naidu, DS
    Heinen, JA
    IEE PROCEEDINGS-CONTROL THEORY AND APPLICATIONS, 2001, 148 (05): : 391 - 396
  • [6] Unified approach to H∞-optimal control of singularly perturbed systems:: Perfect state measurements
    Singh, H
    Brown, RH
    Naidu, DS
    PROCEEDINGS OF THE 37TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4, 1998, : 2214 - 2215
  • [7] Unified H∞ approach for a singularly perturbed aircraft model
    Singh, H
    Naidu, DS
    Nagurka, ML
    PROCEEDINGS OF THE 2000 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 2000, : 1847 - 1851
  • [8] Robust stability of unified singularly perturbed feedback systems
    Singh, H
    Brown, RH
    Naidu, DS
    Heinen, JA
    AIAA GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE, VOLS 1-3: A COLLECTION OF TECHNICAL PAPERS, 1999, : 820 - 825
  • [9] Approximate controller design for singularly perturbed aircraft systems
    Shim, KH
    Sawan, ME
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2005, 77 (04): : 311 - 316
  • [10] Approximate Controller Design for Singularly Perturbed Aircraft Systems
    Graziosi, Joseph E.
    Sawan, M. E.
    Watkins, J. M.
    2014 IEEE 57TH INTERNATIONAL MIDWEST SYMPOSIUM ON CIRCUITS AND SYSTEMS (MWSCAS), 2014, : 161 - 164
12345