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Cheglakov

Flight control of highly maneuverable aircraft during aerial refueling
Engineering Education # 01, January 2013
DOI: 10.7463/0113.0500331
The author considers aircraft flight control during aerial refueling. Results of hardware-in-loop simulation and flight tests are presented in this paper. A corrected model of aerodynamic coupling of a tanker with a receiver is the first main outcome of this study. The control law for the fly-by-wire system’s aerial refueling special mode is another one. This control law ensures desired handling qualities for the aerial refueling task and could be used in fly-by-wire systems. That fact was validated by hardware-in-loop simulation and flight tests. The author’s further study will include development of a control law for the automatic docking procedure during aerial refueling.
 
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