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control and inceptor systems for an aircraft, aircraft, method for controlling a joystick, and tangible computer program product
control and inceptor systems for an aircraft, aircraft, method for controlling a joystick, and tangible computer program product
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机译：飞机的控制和接收器系统，飞机，控制操纵杆的方法和有形的计算机程序产品
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摘要
A control system (400) for an active inceptor (103) is described for an electric cable flight control aircraft that allows a zero force zero point to settle into a non-zero offset compensation position. A state of the internal position of a second order mass spring damper model is moved in conjunction with force-displacement characteristic coordinates. This results in no second-order dynamics being superimposed on the feel of the inceptor 103 during dynamic adjustment of the trim position, thereby eliminating the possibility of any unpleasant humming being felt by the inceptor operator during a trim operation.
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