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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1987, Vol. 8 ›› Issue (4): 171-178.
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Yang Yidong, Wang Jianping
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Abstract: This paper, based on the CCU-YH-16 fighter aircraft,investigates the design philosophy and configuration of the.flight control system with maneuver enhancement and gust alleviation. Comparison between basic flight control system and maneuver enhancement/gust alleviation system is shown by simu lation results.The functions of maneuver enhancement/gust alleviation are examined and evaluated.Parameter optimization method is used using C* flight performance criterion as objective function.
Yang Yidong;Wang Jianping. DESIGN OF FLIGHT CONTROL SYSTEM WITH MANEUVER ENHANCEMENT AND GUST ALLEVIATION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1987, 8(4): 171-178.
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