The RCAM design challenge problem description

摘要: A common control law design problem has been specified based on a military aicraft configuration as part of GARTEUR Action Group AG-08 “Robust Flight Control”. The aircraft mathematical model description is accompanied by set specifications for wide flight envelope law. are mirrored evaluation criteria to facilitate comparison different methods. challenge document also presents participants with list attributes, covering the method, process and resultant controller, which they should report provide balanced assessment complete development their in addition presentation results.