Neural network based dynamic surface control of hypersonic flight dynamics using small-gain theorem.

Bin Xu Qi Zhang Yongping Pan

Published in: Neurocomputing (2016)

Keyphrases

neural network
external disturbances
dynamic model
highly nonlinear
air fuel ratio
control system
small number
dynamic characteristics
nasa langley research center
surface reconstruction
space shuttle
flight test
control method
control strategy
range data
closed loop
d objects
three dimensional