Joint Estimation of Carrier Airwake and Aircraft Dynamics Using Invariant Extended Kalman Filter
Author:
Affiliation:
1. School of Automation Science and Electrical Engineering, Beihang University (BUAA),The Seventh Research Division,Beijing,P.R.China
2. Shenyang Aircraft Design and Research Institute,Shenyang,P.R.China
Funder
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10450150/10449968/10452111.pdf?arnumber=10452111
Reference14 articles.
1. Research on effect airwake acts on glide performance of carrier-based aircraft
2. Automatic Landing for Carrier-Based Aircraft Under the Conditions of Deck Motion and Carrier Airwake Disturbances
3. Flight control and airwake suppression algorithm for carrier landing based on model predictive control
4. Adaptive Super-Twisting Control for Automatic Carrier Landing of Aircraft
5. Estimation of Maneuvering Aircraft States and Time-Varying Wind with Turbulence
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