Nonlinear μ flight control and suboptimal exact solution on F-16 application

被引：0
|
作者：
Department of Aeronautical Engineering, National Defense University, Chung Cheng Institute of Technology, Taoyuan 335, Taiwan [1 ]
不详 [2 ]
不详 [3 ]
机构：
来源：
| 1600年 / 666-671卷 / 2005期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Flight dynamics - Gain control - Parameter estimation - Partial differential equations - Uncertain systems
引用
收藏
相关论文
共 50 条
  • [41] Siding mode control of pitch-rate of an F-16 aircraft
    Aircraft Research and Development Office, Royal Thai Air Force, Bangkok, Thailand
    不详
    World Acad. Sci. Eng. Technol., 2009, (633-639):
  • [42] Nonlinear reconfiguration for asymmetric failures in a six degree-of-freedom F-16
    Thomas, S
    Kwatny, HG
    Chang, BC
    PROCEEDINGS OF THE 2004 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 2004, : 1823 - 1828
  • [43] Parallel evolutionary optimized pitching motion control for F-16 aircraft
    Lee, KH
    Kim, JH
    CEC: 2003 CONGRESS ON EVOLUTIONARY COMPUTATION, VOLS 1-4, PROCEEDINGS, 2003, : 1199 - 1205
  • [44] MMAE-based control redistribution applied to the VISTA F-16
    Stepaniak, MJ
    Maybeck, PS
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1998, 34 (04) : 1249 - 1260
  • [45] EXACT SOLUTION FOR SUBOPTIMAL CONTROL OF NUCLEAR-REACTORS WITH DISTRIBUTED PARAMETERS
    KIM, SH
    CHANG, J
    NUCLEAR SCIENCE AND ENGINEERING, 1981, 78 (02) : 171 - 175
  • [46] MMAE-based control redistribution applied to the VISTA F-16
    Stepaniak, MJ
    Maybeck, PS
    PROCEEDINGS OF THE 1997 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 1997, : 133 - 139
  • [47] Application of a three-field nonlinear fluid-structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter
    Farhat, C
    Geuzaine, P
    Brown, G
    COMPUTERS & FLUIDS, 2003, 32 (01) : 3 - 29
  • [48] Condensation on ONERA M6 and F-16 wings in atmospheric flight: Numerical modeling
    Goodheart, Kevin A.
    Schnerr, Günter H.
    Journal of Aircraft, 1600, 42 (02): : 402 - 412
  • [49] F-16/BRU-55 flight vibration data collection using digital recorders
    Fling, SA
    Binkley, K
    Wrenne, D
    JOURNAL OF THE IEST, 1999, 42 (01): : 41 - 45
  • [50] Output tracking for nonlinear non-minimum phase systems with output delay and application to an F-16 jet fighter
    Zhu, Bo
    Wang, Xinhua
    Cai, Kai-Yuan
    INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2011, 42 (03) : 529 - 538
12345