| 摘要 |
PROBLEM TO BE SOLVED: To provide a airframe control device performing the twin steering of the same phase, which keeps the response of high acceleration control even when a steering angle is saturated, and keeps superior flying performance. SOLUTION: This control device is provided with an autopilot for calculating a front wing steering angle command signal and a rear wing steering angle command signal on the basis of inputted acceleration command signal, an acceleration signal and an angular speed signal, and outputting a corrected front wing steering angle command signal obtained by correcting the front wing steering angle command signal on the basis of the rear wind steering angle command signal to a front steering device, and the rear wind steering angle command signal to the rear steering device, and a rear wing restricting device for reducing a rear wind steering angle by subtracting an adjustment command signal calculated on the basis of the corrected front wing steering angle command signal, a predetermined value, and an adjustment coefficient from the rear wing steering angle command signal. Whereby a rear wing can be returned by the rear wing restricting device when the front wing steering angle starts its saturation, and the moment is generated to a high elevation angle by increasing the lifting of the front wing by decreasing the lifting of the rear wing, which improves the response, and the flying performance. COPYRIGHT: (C)2003,JPO
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