TY - GEN
T1 - Several models of artificial inteligence elements for airctaft control
AU - Goncharenko, A. V.
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/12/14
Y1 - 2016/12/14
N2 - It is made an attempt to find some optimal measure for the coefficient of a proportional governor augmentation in the aircraft navigation and motion linear model inertness-less object control system as continuous alternatives individual preferences densities distributions, using the preferences subjective entropy maximum principle, proposed by Professor V.A. Kasianov (National Aviation University, Kyiv, Ukraine) in case of one and two-dimensions. It is obtained the continuous alternative preferences distribution densities; this together with the preferences distributions for the predetermined time points allows making the optimal choice of the available aircraft navigation. Theoretical speculations are illustrated with the example calculation experiments. The necessary diagrams are plotted.
AB - It is made an attempt to find some optimal measure for the coefficient of a proportional governor augmentation in the aircraft navigation and motion linear model inertness-less object control system as continuous alternatives individual preferences densities distributions, using the preferences subjective entropy maximum principle, proposed by Professor V.A. Kasianov (National Aviation University, Kyiv, Ukraine) in case of one and two-dimensions. It is obtained the continuous alternative preferences distribution densities; this together with the preferences distributions for the predetermined time points allows making the optimal choice of the available aircraft navigation. Theoretical speculations are illustrated with the example calculation experiments. The necessary diagrams are plotted.
KW - Active navigation and motion control
KW - Adaptation
KW - Aircraft flight control
KW - Artificial intellect
KW - Continuous alternative
KW - Extremal
KW - Optimal choice
KW - Optimization
KW - Preferences distribution density
KW - Subjective entropy maximum principle
KW - Variational problem
UR - https://www.scopus.com/pages/publications/85010402980
U2 - 10.1109/MSNMC.2016.7783148
DO - 10.1109/MSNMC.2016.7783148
M3 - 会议稿件
AN - SCOPUS:85010402980
T3 - 2016 IEEE 4th International Conference Methods and Systems of Navigation and Motion Control, MSNMC 2016 - Proceedings
SP - 224
EP - 227
BT - 2016 IEEE 4th International Conference Methods and Systems of Navigation and Motion Control, MSNMC 2016 - Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 4th IEEE International Conference Methods and Systems of Navigation and Motion Control, MSNMC 2016
Y2 - 18 October 2016 through 20 October 2016
ER -