科研之友
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摘要
The objective of this paper is applying the Time Delay Control scheme for the aircraft auto-landing guidance problem A stability and control augmentation system and longitudinal auto landing guidance law using Time delay Control is proposed and evaluated through a simulation with model uncertainties and wind disturbances The proposed Time Delay Control guidance law shows good performance and is robust to model uncertainties and disturbances
- 出版日期2010-11
