Modular Control Law Design for the Innovative Control Effectors (ICE) Tailless Fighter Aircraft Configuration 101-3
作者： James F. Buffington
DOI: 10.21236/ADA374954
关键词: Inversion (meteorology) 、 Flight envelope 、 Flight simulator 、 Engineering 、 Modular design 、 Control theory 、 Control system 、 Redundancy (engineering) 、 Inversion of control 、 Linear programming 、 Control engineering 、 Law
摘要: Abstract : A modular flight control system is developed for a tailless fighter aircraft with innovative effectors. Dynamic inversion synthesis used to develop full envelope law, Minor dynamic command variable revisions are required due the nature of configuration studied achieve nominal stability and performance. Structured singular value simulation analysis shows that robust achieved performance slightly deficient modeling errors. multi-branch linear programming-based method allocation redundant limited
sci-hub.st 参考文章(1)
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