Control Method Research on Aerocraft with Rapid Changing Parameters

Flying qualities of aerocraft are closely related to the performance of control system. Aimed at the roll stable aerocraft with rapid changing parameters, on the basis of analyzing the typical trajectory, and taking pitch control loop for an example, a three loop autopilots of roll stability, pitch and yaw were designed. http://www.sj-ce.org/paperInfo.aspx?ID=374

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Last Updated October 10, 2013, 20:22 (UTC)
Created May 14, 2013, 07:27 (UTC)