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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1998, Vol. 19 ›› Issue (S1): 113-115.
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Wang Shaoping, Li Peiqiong, Pei Ying
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Abstract: This paper provides a function reconfiguration method. Under the rule of "effective source never give up", this paper proposes a function reconfiguration method for actuators. The pseudo inverse method is applied to investigate the function reconfiguration for the rudder fault mode of a flight control system. The simulation results indicate that the method is effective.
Key words: function r econfiguration, pseudo-inverse method, flight contr ol systems
CLC Number:
V249
Wang Shaoping;Li Peiqiong;Pei Ying. STUDY ON FUNCTION RECONFIGURATION OF FLIGHT CONTROL SYSTEMS[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1998, 19(S1): 113-115.
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https://hkxb.buaa.edu.cn/EN/Y1998/V19/IS1/113