Aircraft Longitudinal Auto-landing Guidance Law Using Time Delay Control Scheme
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
- Publisher
- JAPAN SOC AERONAUT SPACE SCI
- Issue Date
- 2010-11
- Language
- English
- Article Type
- Article
- Keywords
ROBOT
- Citation
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.53, no.181, pp.207 - 214
- ISSN
- 0549-3811
- Appears in Collection
- EE-Journal Papers(저널논문)
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