EXTENSION OF AN AEROELASTIC PARAMETER FOR ESTIMATION OF THE EFFECTS OF FLEXIBILITY ON THE LATERAL STABILITY AND CONTROL OF AIRCRAFT

被引：0
|
作者：
RODDEN, WP
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 08期
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：624 / 625
页数：2
相关论文
共 50 条
  • [31] Adaptive Control of a Civil Aircraft Through On-Line Parameter Estimation
    Ferreres, G.
    Hardier, G.
    Seren, C.
    2016 3RD CONFERENCE ON CONTROL AND FAULT-TOLERANT SYSTEMS (SYSTOL), 2016, : 798 - 804
  • [32] Real-time parameter estimation for reconfigurable control of unstable aircraft
    Kamali, C.
    Pashilkar, A. A.
    Raol, J. R.
    DEFENCE SCIENCE JOURNAL, 2007, 57 (04) : 527 - 537
  • [33] Modelling and parameter estimation for fly-by-wire aircraft/control systems
    Jitendra R Raol
    G Girija
    Sadhana, 1999, 24 : 97 - 119
  • [34] Real-time parameter estimation for reconfigurable control of unstable aircraft
    National Aerospace Laboratories, Bangalore-560 017, India
    Def Sci J, 2007, 4 (527-537):
  • [35] Lateral Aircraft Parameter Estimation Using Neuro-Fuzzy and Genetic Algorithm Based Method
    Roy, Abhishek Ghosh
    Peyada, N. K.
    2017 IEEE AEROSPACE CONFERENCE, 2017,
  • [36] Aircraft lateral linear parameter varying model predictive control with time varying weight
    Zhu, Qi-Dan
    Wang, Li-Peng
    Zhang, Zhi
    Wen, Zi-Xia
    Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2015, 32 (01): : 101 - 109
  • [37] Optimal input design for online parameter estimation for aircraft with multiple control surfaces
    Han, Yongsu
    Kim, Youdan
    ENGINEERING OPTIMIZATION, 2011, 43 (05) : 559 - 580
  • [38] Parameter Estimation Based Control of Hypersonic Aircraft with Magnitude Constraints on States and Actuators
    Xu, Bin
    Wang, Shixing
    Gao, Daoxiang
    2013 INTERNATIONAL CONFERENCE ON UNMANNED AIRCRAFT SYSTEMS (ICUAS), 2013, : 875 - 880
  • [39] STABILITY BOUNDARIES FOR AIRCRAFT WITH UNSTABLE LATERAL-DIRECTIONAL DYNAMICS AND CONTROL SATURATION
    SHRIVASTAVA, PC
    STENGEL, RF
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1989, 12 (01) : 62 - 70
  • [40] Grid-Based and Polytopic Linear Parameter-Varying Modeling of Aeroelastic Aircraft with Parametric Control Surface Design
    Mocsanyi, Reka Dora
    Takarics, Bela
    Kotikalpudi, Aditya
    Vanek, Balint
    FLUIDS, 2020, 5 (02)
12345