Method for determining using priority of each control surface of multi-control-surface aircraft during over-the-horizon stage
A technology with multiple control surfaces and control surfaces, applied in the field of flight control, can solve the problems of slow response of aircraft control, affecting the flight performance of the aircraft, affecting the flight quality and agility of the aircraft, and achieve the effect of reducing adverse costs and improving flight performance.
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[0017] Refer to attached figure 1 In this embodiment, the method of the present invention is used to determine the use priority of each control surface of a certain type of multi-control surface aircraft in the over-the-horizon air combat stage. In the embodiment, the control surfaces suitable for use by the multi-control surface aircraft in the over-the-horizon air combat stage include: the right close-coupled canard 1, the left close-coupled canard 2, the right outer elevon 3, and the left outer elevon 4. The right inner elevon 5, the left inner elevon 6 and the rudder. Since the rudder is the only heading control surface, it is not necessary to determine its deflection angle through the control allocation process, so it is necessary to determine the priority of use in this embodiment. The control surfaces of the stage are the right near-coupled canard 1, the left near-coupled canard 2, the right outer elevon 3, the left outer elevon 4, the right inner elevon 5 and the left ...
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