Simulation modeling method for composite flight strategy of flapping wing air vehicle

A flapping-wing aircraft and flight strategy technology, applied in the aerospace field, can solve problems such as unfavorable, limited simulation, research on the flight performance of flapping-wing aircraft, and achieve the effect of high simulation

Inactive Publication Date: 2016-06-15
NORTHWESTERN POLYTECHNICAL UNIV
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AI Technical Summary

Problems solved by technology

At present, the established flapping-wing aircraft simulation model can only simulate the state of the flapping-wing aircraft flying at a constant speed, but cannot realize the composite flight state of flapping-gliding similar to birds. The

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  • Simulation modeling method for composite flight strategy of flapping wing air vehicle
  • Simulation modeling method for composite flight strategy of flapping wing air vehicle
  • Simulation modeling method for composite flight strategy of flapping wing air vehicle

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Embodiment Construction

[0050] In order to make the technical problems, technical solutions and beneficial effects solved by the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0051] Compound flight refers to: flapping-gliding-flapping, namely: including the normal flapping state, the transitional state from flapping to gliding, the gliding state, the transitional state from gliding to flapping, and returning to the normal flapping state. Therefore, compound flight is different from conventional flight state with constant flapping frequency and constant flapping amplitude. Composite flight and the actual flight state of birds are more realistic. Establishing a simulation model of a flapping-wing aircraft with a composite flight state can study...

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Abstract

The invention provides a simulation modeling method for a composite flight strategy of a flapping wing air vehicle. The method comprises following steps: obtaining basic parameters of a flapping wing air vehicle under study; establishing an aero-dynamic model; establishing a dynamic model; describing composite flight process; establishing the relation between flight power and flapping power and flapping amplitude to obtain a flight energy consumption calculation model; establishing a control rate model; linking and sorting the aero-dynamic model, the dynamic model, a composite flight planning model, the flight energy consumption calculation model and the control rate model to establishing a final simulation model. The advantages of the method are: simulation technicists can efficiently use the Matlab/Simulink simulation environment to establish a composite flight simulation model of a flapping wing air vehicle and determine composite flight ability of the flapping wing are vehicle through analyzing simulation results of different flight strategies, and find an optimal flight strategy; the method is of instructive importance to flapping wing air vehicle engineering improvement.

Description

technical field [0001] The invention belongs to the technical field of aerospace, and in particular relates to a compound flight strategy simulation modeling method of a flapping-wing aircraft. Background technique [0002] Flapping Wing Micro Air Vehicle (FMAV for short) is a small, light-weight aircraft that carries micro-sensors for reconnaissance and surveillance, and uses flapping wings as a power plant. Micro-flapping-wing aircraft has broad application prospects in military and civilian applications, and has become a hot topic in the field of micro-aircraft research in various countries in the past ten years. With the advancement of the research on the flight mechanism of birds, the rapid development of related fields such as micro-electromechanical technology (MEMS) and new materials, the research level of bionic flapping-wing aircraft is also constantly improving. [0003] It is one of the important approaches in the research of flapping-wing aircraft to simulate a...

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Application Information

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IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 钟京洋宋笔锋杨文青付鹏张红梅唐伟薛栋梁少然年鹏
Owner NORTHWESTERN POLYTECHNICAL UNIV
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