Transformation wing aircraft energy management method based on dynamic flight

Abstract

The invention discloses a transformation wing aircraft energy management method based on dynamic flight. A transformation wing aircraft flies in a fixed wing flight mode after entering a gradient windfield at the preset height, a dynamic flight optimized path is adopted in the fixed wing flight mode, and therefore the aircraft flies in a Rayleigh ring mode. The transformation wing aircraft obtains energy in the against-wind ascending process and the following-wind descending process, the energy supplements the energy consumed in the turning process, and long-distance flight of the transformation wing aircraft is achieved.

Description

technical field [0001] The invention relates to the field of energy management of deformable wing aircraft, in particular to an energy management method of deformable wing aircraft based on dynamic soaring. Background technique [0002] Most of the current aircraft are fixed-wing aircraft and flapping-wing aircraft. These two wing layouts have their own advantages. Fixed-wing aircraft are widely used, mainly relying on propellers or turbine engines to generate thrust, and fixed wings generate lift to fly. Therefore Its flight speed is fast, relatively economical, and its carrying capacity is large, but its mechanical efficiency is not high; while the flapping wing aircraft generates lift and thrust at the same time through the flapping of the wing surface, which has the advantages of high efficiency, small size and light weight, and can be applied In military reconnaissance, environmental recognition and other aspects. [0003] Aircraft flying in the sky consumes a lot of e...

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