Neural Networks for Air Data Estimation: Test of Neural Network Simulating Real Flight Instruments

被引:0
作者
Battipede, Manuela [1 ]
Gili, Piero [1 ]
Lerro, Angelo [1 ]
机构
[1] Politecn Torino, Dept Mech & Aerosp Engn, I-10129 Turin, Italy
来源
ENGINEERING APPLICATIONS OF NEURAL NETWORKS | 2012年 / 311卷
关键词
Neural network; turbulence; noise; air data;
D O I
暂无
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
In this paper virtual air data sensors have been modeled using neural networks in order to estimate the aircraft angles of attack and sideslip. These virtual sensors have been designed and tested using the aircraft mathematical model of the De Havilland DHC-2. The aim of the work is to evaluate the degradation of neural network performance, which is supposed to occur when real flight instruments are used instead of simulated ones. The external environment has been simulated, and special attention has been devoted to electronic noise that affects each input signals examining modern devices.. Neural networks, trained with noise free signals, demonstrate satisfactory agreement between theoretical and estimated angles of attack and sideslip.
引用
收藏
页码:282 / 294
页数:13
相关论文
共 23 条
  • [1] [Anonymous], 1996, Building Neural Networks
  • [2] Calia A., 2008, IEEE INT S IND EL IS
  • [3] DEFENSE D.O., MILSTD810E
  • [4] di Fusco C., 2006, RICOSTRUZIONE ANGOLI
  • [5] Etkin B., 1982, DYNAMICS FLIGHT STAB
  • [6] Gladiator Technologies I, 2011, HIGH PERF MEMS AHRS
  • [7] Haering E.A., 1995, AIRDATA MEASUREMENT
  • [8] McCool K., NEURAL NETWORK SYSTE
  • [9] Napolitano M. R., 2000, AIRCRAFT DESIGN, V3, P103, DOI DOI 10.1016/51369-8869(00)00009-4
  • [10] Norgaard M., 2003, NNSYSID TOOLBOX USE