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A attitude control method of insect-like flapping-wing aircraft based on fuzzy neural network

A fuzzy neural network and flapping aircraft technology, applied in the field of aeronautical engineering aircraft, can solve the problem of less research work

Active Publication Date: 2020-03-17
SHANGHAI JIAOTONG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the fuzzy neural network has been applied in some engineering fields, such as controlling the temperature of the heating furnace, estimating the state of the battery and predicting the traffic flow, etc., but there is still relatively little research work on the flight control of the flapping wing aircraft.

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  • A attitude control method of insect-like flapping-wing aircraft based on fuzzy neural network
  • A attitude control method of insect-like flapping-wing aircraft based on fuzzy neural network
  • A attitude control method of insect-like flapping-wing aircraft based on fuzzy neural network

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Embodiment

[0060] The invention proposes an attitude control method of a bionic flapping-wing aircraft based on a type-two fuzzy neural network in a triangular uncertain central interval. Specific control codes can be integrated in the onboard embedded flight control unit.

[0061] Such as figure 1 As shown, the uncertain central interval type II triangular fuzzy membership function used in the present invention is introduced as follows:

[0062] The interval type-2 triangular fuzzy membership function is an extension of the traditional type-1 triangular fuzzy membership function. The value of the traditional type I triangular fuzzy membership function is a clear number. But the value of interval type-two triangular fuzzy membership function is still type-one fuzzy set. This means that it has a stronger ability to express uncertainty than the type I triangular fuzzy membership function. attached figure 1 is a schematic diagram of the membership function of the uncertainty center int...

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Abstract

The invention relates to an insect flapping wing-like aircraft attitude control method based on a type-2 fuzzy neural network of a triangular uncertain central interval. The method comprises the following steps that 1, initial parameters of a proportional plus derivative controller and the fuzzy neural network in an insect flapping wing-like aircraft attitude control model are set; 2, flapping wing aircraft attitude angle information is acquired, and after filter fusion is conducted, an attitude angle measured practically is obtained; 3, difference between the attitude angle measured practically and a preset attitude angle is calculated to obtain a corresponding attitude angle error and a first derivative of the attitude angle error, the corresponding attitude angle error and the first derivative of the attitude angle error are used as input quantities of the proportional plus derivative controller and the fuzzy neural network, output of the controller is obtained, and meanwhile, the parameters of the fuzzy neural network are updated; 4, an insect flapping wing-like aircraft airborne flight control unit adjusts the attitude angle according to output of the proportional plus derivative controller and the fuzzy neural network. Compared with the prior art, the insect flapping wing-like aircraft attitude control method based on the type-2 fuzzy neural network of the triangular uncertain central interval has the advantages of being high in anti-jamming capability, high in robustness, high in convenience and practicability and the like.

Description

technical field [0001] The invention relates to the field of aeronautical engineering aircraft, in particular to an attitude control method of an insect-imitating flapping-wing aircraft based on a triangular uncertain central interval type-two fuzzy neural network. Background technique [0002] In the past few years, insect-like flapping-wing micro-aircraft has become a research hotspot in the field of bionic engineering because of its small size, light weight, compact structure, quiet flight, and high maneuverability. These advantages make it applicable to many practical engineering fields. For example, search and rescue inside buildings or in collapsed structures; sensing chemical spills; radiation monitoring of nuclear power plants; and surveillance and reconnaissance during military operations. With the advancement of micro-motors, on-board power supplies and sensors, and rigid and flexible transmission mechanisms, the manufacture of insect-like flapping-wing micro-airc...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08G05B13/04
CPCG05B13/0285G05B13/042G05D1/0825
Inventor 张超张各各姚瑞文张卫东陆宇曹刚
Owner SHANGHAI JIAOTONG UNIV
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