Dynamic inversion: an evolving methodology for flight control design
作者： DALE ENNS , DAN BUGAJSKI , RUSS HENDRICK , GUNTER STEIN
DOI: 10.1080/00207179408923070
关键词:
摘要: This paper describes nonlinear dynamic inversion as an alternative design method for flight controls. The is illustrated with super-manoeuvring control laws the F-18 high angle-of-attack research vehicle.
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