HIGH-ALPHA AERODYNAMIC MODEL IDENTIFICATION OF T-2C AIRCRAFT USING THE EBM METHOD

被引：17
|
作者：
STALFORD, HL
机构：
来源：
JOURNAL OF AIRCRAFT | 1981年 / 18卷 / 10期
关键词：
D O I：
10.2514/3.57565
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：801 / 809
页数：9
相关论文
共 50 条
  • [1] Aircraft damage detection and identification using the aerodynamic model
    Ruangwiset, A.
    Sakurai, A.
    Memoirs of the Graduate School of Engineering, Kyushu University, 2000, 60 (02): : 91 - 103
  • [2] Flight Testing of a Dynamically Scaled Transport Aircraft Model for High-Alpha Wind Tunnel Data Validation
    Pusztai, Daniel
    Lowenberg, Mark H.
    Neild, Simon A.
    AIAA SCITECH 2024 FORUM, 2024,
  • [3] Identification of Aerodynamic Derivatives of a Flexible Aircraft using Output Error Method
    Majeed, M.
    Kar, Indra Narayan
    MECHANICAL AND AEROSPACE ENGINEERING, PTS 1-7, 2012, 110-116 : 5328 - +
  • [4] Aerodynamic parameter identification for aircraft wing icing using H∞ method
    Ding, Di
    Che, Jing
    Qian, Weiqi
    Wang, Qing
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2018, 39 (03):
  • [5] Aircraft Lateral-Directional Aerodynamic Parameter Identification and Solution Method Using Segmented Adaptation of Identification Model and Flight Test Data
    Wang, Lixin
    Zhao, Rong
    Zhang, Yi
    AEROSPACE, 2022, 9 (08)
  • [6] Identification and Modeling Method of Longitudinal Stall Aerodynamic Parameters of Civil Aircraft Based on Improved Kirchhoff Stall Aerodynamic Model
    Wang, Lixin
    Zhao, Rong
    Xu, Ke
    Zhang, Yi
    Yue, Ting
    AEROSPACE, 2023, 10 (04)
  • [7] Online Aerodynamic Model Identification Using a Recursive Sequential Method for Multivariate Splines
    Sun, L. G.
    de Visser, C. C.
    Chu, Q. P.
    Mulder, J. A.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2013, 36 (05) : 1278 - 1288
  • [8] A blended method incorporating a multi-model for pulse wind tunnel aerodynamic identification considering large-scale aircraft
    Li, Shichao
    Wang, Qinchao
    Ma, Guilin
    Gao, Hongli
    Guo, Liang
    Liu, Zihao
    Shao, Kaibo
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2023, 34 (01)
  • [9] Robust identification method for nonlinear model structures and its application to high-performance aircraft
    Shi, Zhong-Ke
    Wu, Fang-Xiang
    INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2013, 44 (06) : 1040 - 1051
  • [10] Identification of Noise Sources in an Aircraft Fuselage Using an Inverse Method Based on a Finite Element Model
    Kletschkowski, Thomas
    Weber, Matthias
    Sachau, Delf
    ACTA ACUSTICA UNITED WITH ACUSTICA, 2011, 97 (06) : 974 - 983
12345