In this paper, adaptive critic based neural networks have been used to design a controller for a benchmark problem in aircraft autolanding. The adaptive critic control methodology comprises successive adaptations of two neural networks, namely `action' and `critic' networks until closed loop optimal control is achieved. The autolanding problem deals with longitudinal dynamics of an aircraft which is to be landed in a specified touchdown region in the presence of wind disturbances and gusts using elevator deflection as the control for glideslope and flare modes. The performance of the neurocontroller is compared to that of a conventional PID controller. Neurocontroller's capabilities are further explored by making it more generic and versatile in the sense that the glideslope angle can be changed at will during the landing process. Flight paths (trajectories) obtained for a wide range of glideslope angles in presence of wind gusts are compared with the optimal flight paths which are obtained by solving the linear quadratic regulator formulation using conventional optimal control theory
G. Saini and S. N. Balakrishnan, "Adaptive Critic Based Neurocontroller for Autolanding of Aircraft with Varying Glideslopes," Proceedings of the International Conference on Neural Networks,1997, Institute of Electrical and Electronics Engineers (IEEE), Jan 1997.
The definitive version is available at https://doi.org/10.1109/ICNN.1997.614409
International Conference on Neural Networks,1997
Mechanical and Aerospace Engineering
Keywords and Phrases
Adaptive Critic; Aircraft; Aircraft Landing Guidance; Attitude Control; Autolanding; Closed Loop System; Closed Loop Systems; Glideslopes; Learning Systems; Longitudinal Dynamics; Neural Networks; Neurocontrollers; Optimal Control; Wind Disturbances
Article - Conference proceedings
© 1997 Institute of Electrical and Electronics Engineers (IEEE), All rights reserved.
01 Jan 1997