Journal
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
Volume 54, Issue 6, Pages 2662-2674Publisher
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TAES.2018.2826398
Keywords
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Funding
- National Natural Science Foundation of China [61741313, 61673209, 61533008]
- Aeronautical Science Foundation [2016ZA52009]
- Fundamental Research Funds for the Central Universities [NS2017015]
- Foundation of Graduate Innovation Center in NUAA [kfjj20170306]
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This paper studies the automatic carrier landing control problem of aircrafts with the system dynamics of nonlinearity and multivariable coupling, by applying preview control scheme. An automatic carrier landing system is developed, including a particle filtering based flight deck motion prediction, a corrected reference glide slope generation and an integrated guidance and control modules. A preview control algorithm is presented to guarantee the optimal tracking performance, and simulations demonstrate the better carrier landing performance under the deck motion and airwake disturbances, comparing with the proportional-integral-derivative control scheme.
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