Experimental Analysis of Neural Approaches for Synthetic Angle-of-Attack Estimation

被引:4
|
作者
Lerro, Angelo [1 ]
Gili, Piero [1 ]
Fravolini, Mario Luca [2 ]
Napolitano, Marcello [3 ]
机构
[1] Polytech Univ Turin, Dept Mech & Aerosp Engn, Cso Duca Abruzzi 24, I-10129 Turin, Italy
[2] Univ Perugia, Dept Elect & Informat Engn, Via G Duranti 93, I-06125 Perugia, Italy
[3] West Virginia Univ, Dept Mech & Aerosp Engn, POB 6106, Morgantown, WV 26506 USA
关键词
NETWORK ALGORITHM; NOISE-IMMUNITY;
D O I
10.1155/2021/9982722
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Synthetic sensors enable flight data estimation without devoted physical sensors. Within modern digital avionics, synthetic sensors can be implemented and used for several purposes such as analytical redundancy or monitoring functions. The angle of attack, measured at air data system level, can be estimated using synthetic sensors exploiting several solutions, e.g., model-based, data-driven, and model-free state observers. In the class of data-driven observers, multilayer perceptron neural networks are widely used to approximate the input-output mapping angle-of-attack function. Dealing with experimental flight test data, the multilayer perceptron can provide reliable estimation even though some issues can arise from noisy, sparse, and unbalanced training domain. An alternative is offered by regularization networks, such as radial basis function, to cope with training domain based on real flight data. The present work's objective is to evaluate performances of a single-layer feed-forward generalized radial basis function network for AoA estimation trained with a sequential algorithm. The proposed analysis is performed comparing results obtained using a multilayer perceptron network adopting the same training and validation data.
引用
收藏
页数:13
相关论文
共 50 条
  • [31] A neural computing based approximate inverse system and application to high angle-of-attack control of aircraft
    Li, Chunwen
    Zou, Xinsheng
    Cui, Guang-zhao
    Jin, Nan
    Cai, Lingzhi
    DYNAMICS OF CONTINUOUS DISCRETE AND IMPULSIVE SYSTEMS-SERIES B-APPLICATIONS & ALGORITHMS, 2007, 14 : 207 - 212
  • [32] DISTRIBUTION OF AIR DENSITY NEAR SUPERSONIC CONE AT AN ANGLE-OF-ATTACK
    MENDE, NP
    PODLASKIN, AB
    ZHURNAL TEKHNICHESKOI FIZIKI, 1994, 64 (07): : 9 - 20
  • [33] WAKES OF 3-AXISYMMETRICAL BODIES AT ZERO ANGLE-OF-ATTACK
    ILDAY, O
    ACAR, H
    ELBAY, MK
    ATLI, V
    AIAA JOURNAL, 1993, 31 (06) : 1152 - 1154
  • [34] Design Of VSC For Overload Control In High Angle-of-attack Missile
    Liang, Xuechao
    Yang, Jun
    Qiu, Feng
    2013 IEEE INTERNATIONAL CONFERENCE OF IEEE REGION 10 (TENCON), 2013,
  • [35] HIGH ANGLE-OF-ATTACK AERODYNAMICS ON A SLENDER BODY WITH A JET PLUME
    NELSON, RC
    FLEEMAN, EL
    JOURNAL OF SPACECRAFT AND ROCKETS, 1975, 12 (01) : 12 - 16
  • [36] NONLINEAR CONTROL LAW WITH APPLICATION TO HIGH ANGLE-OF-ATTACK FLIGHT
    BUGAJSKI, DJ
    ENNS, DF
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) : 761 - 767
  • [37] SOUND FROM A PROPELLER AT ANGLE-OF-ATTACK - A NEW THEORETICAL VIEWPOINT
    HANSON, DB
    PROCEEDINGS OF THE ROYAL SOCIETY-MATHEMATICAL AND PHYSICAL SCIENCES, 1995, 449 (1936): : 315 - 328
  • [38] WAKES OF 3 AXISYMMETRICAL BODIES AT ZERO ANGLE-OF-ATTACK - REPLY
    ILDAY, O
    ACAR, H
    ELBAY, MK
    ATLI, V
    AIAA JOURNAL, 1995, 33 (03) : 570 - 570
  • [39] Effect of thickness and angle-of-attack on the aeroelastic stability of supersonic fins
    Firouz-Abadi, R. D.
    Alavi, S. M.
    AERONAUTICAL JOURNAL, 2012, 116 (1182): : 777 - 792
  • [40] EXTENSION OF EQUIVALENT ANGLE-OF-ATTACK METHOD FOR NONLINEAR FLOWFIELDS.
    Hemsch, M.J.
    Nielsen, J.N.
    1600, (22):