Abstract
The objective of this paper is applying the Time Delay Control scheme for the aircraft auto-landing guidanceproblem. A stability and control augmentation system and longitudinal auto-landing guidance law, using Time DelayControl, is proposed and evaluated through a simulation with model uncertainties and wind disturbances. The proposedTime Delay Control guidance law shows good performance and is robust to model uncertainties and disturbances.Key Words: Aircraft, Guidance and Control, Auto-landing, Time Delay Control, Turbulence
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