Robust Aeroelastic Response Estimation for Flexible Aircraft

被引:0
|
作者
Mahapatra, Lagnesh [1 ]
Halbe, Omkar [2 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Bombay 400076, Maharashtra, India
[2] CSIR, Natl Aerosp Labs, Flight Mech & Control Div, Bangalore 560017, Karnataka, India
来源
IFAC PAPERSONLINE | 2024年 / 57卷
关键词
aeroelasticity; flexible aircraft; observer; state estimation;
D O I
10.1016/j.ifacol.2024.05.017
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Elastic deformations of flexible aircraft significantly affect its stability, control, and performance. This paper proposes an observer-based approach to estimate the elastic motion of flexible aircraft under uncertainty. Based on an accurate aeroelastic model and primary sensors providing reliable rigid-body measurements, two full-order observers are synthesized to estimate both rigid-body and elastic modes. The first is a classical Luenberger observer with pole placement method for the observer gain selection. The second is a full-order discontinuous sliding mode observer that is robust to bounded exogenous disturbance, such as gust effects. The observer-based approach is demonstrated on a generic flexible hypersonic aircraft model to robustly estimate longitudinal elastic deformation in the presence of moderate gusts.
引用
收藏
页码:95 / 100
页数:6
相关论文
共 50 条
  • [21] Validation Studies for Aeroelastic Trim and Stability Analysis of Highly Flexible Aircraft
    Sotoudeh, Zahra
    Hodges, Dewey H.
    Chang, Chong-Seok
    JOURNAL OF AIRCRAFT, 2010, 47 (04): : 1240 - 1247
  • [22] Reduced-Order Aeroelastic Models for Dynamics of Maneuvering Flexible Aircraft
    Hesse, Henrik
    Palacios, Rafael
    AIAA JOURNAL, 2014, 52 (08) : 1717 - 1732
  • [23] Nonlinear Aeroelastic Trim of Very Flexible Aircraft Described by Detailed Models
    Riso, Cristina
    Di Vincenzo, Fausto G.
    Ritter, Markus
    Cesnik, Carlos E. S.
    Mastroddi, Franco
    JOURNAL OF AIRCRAFT, 2018, 55 (06): : 2338 - 2346
  • [24] Nonlinear Aeroelastic Control of Very Flexible Aircraft Using Model Updating
    Wang, Yinan
    Wynn, Andrew
    Palacios, Rafael
    JOURNAL OF AIRCRAFT, 2018, 55 (04): : 1551 - 1563
  • [25] Aeroelastic trim and flight loads analysis of flexible aircraft with large deformations
    Chao Yang
    LiBo Wang
    ChangChuan Xie
    Yi Liu
    Science China Technological Sciences, 2012, 55 : 2700 - 2711
  • [26] Nonlinear Flight Dynamics of a Flexible Aircraft Subjected to Aeroelastic and Gust Loads
    Fazelzadeh, S. A.
    Sadat-Hoseini, H.
    JOURNAL OF AEROSPACE ENGINEERING, 2012, 25 (01) : 51 - 63
  • [27] Aeroelastic trim and flight loads analysis of flexible aircraft with large deformations
    Yang Chao
    Wang Libo
    Xie ChangChuan
    Liu Yi
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2012, 55 (10) : 2700 - 2711
  • [28] Robust gust load alleviation for a flexible aircraft
    Aouf, N., 1600, CASI, Ottawa, Canada (46):
  • [29] Geometrically Nonlinear Effects on the Aeroelastic Response of a Transport Aircraft Configuration
    Cea, Alvaro
    Palacios, Rafael
    JOURNAL OF AIRCRAFT, 2023, 60 (01): : 205 - 220
  • [30] Unsteady aerodynamic forces and aeroelastic response for external store of an aircraft
    Tang, D
    Dowell, EH
    JOURNAL OF AIRCRAFT, 1998, 35 (05): : 678 - 687