A Control Method for Gust Mitigation of Fixed-wing Aircraft Combining Active and Passive
A control method and fixed-wing technology, applied in the field of aircraft control, can solve problems such as large weight, feedback time lag, and insufficient control efficiency, and achieve the effects of overload and deformation weakening, increased efficiency, and reduced rudder deflection angle
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[0048] The specific implementation method of the present invention will be described in detail below in conjunction with the accompanying drawings.
[0049] A kind of active and passive combination of the control method of fixed-wing aircraft gust mitigation of the present invention, such as figure 1 As shown, the specific steps are as follows:
[0050] Step 1. For a fixed-wing aircraft, construct the two-dimensional coordinate system OZX required for dynamic modeling describing wing deformation;
[0051] Step 2, the wing of the fixed-wing aircraft is divided into an inner wing and a full-motion wingtip, and the full-motion wingtip serves as a passive gust mitigation device and is connected to the inner wing through a torsion shaft.
[0052] Such as figure 2 As shown, the wing of the fixed-wing aircraft is divided into two parts, the inner wing 3 and the full-moving wingtip 1, wherein the full-moving wingtip 1 is a passive gust mitigation device connected to the inner wing ...
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