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Fixed-wing unmanned aerial vehicle rolling maneuvering control method

A control method and unmanned aerial vehicle technology, applied in the direction of attitude control, etc., can solve the problems of inability to switch between forward flight and inverted flight state, lack of fast maneuvering target simulation ability, and inability to realize rapid rollover maneuvering flight actions, etc.

Active Publication Date: 2019-04-16
ZHEJIANG UNIV
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  • Application Information

AI Technical Summary

Problems solved by technology

However, the existing main high-speed unmanned target drones in my country lack the ability to simulate fast maneuvering targets, and cannot flexibly switch between forward and inverted flight states, let alone achieve fully autonomous rapid rollover maneuvers. Therefore, research The rolling maneuver control method of fixed-wing unmanned aerial vehicles has very urgent needs and important significance

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  • Fixed-wing unmanned aerial vehicle rolling maneuvering control method
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  • Fixed-wing unmanned aerial vehicle rolling maneuvering control method

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Embodiment Construction

[0049] The present invention will be further elaborated and illustrated below in conjunction with the accompanying drawings and specific embodiments. The technical features of the various implementations in the present invention can be combined accordingly on the premise that there is no conflict with each other.

[0050] The invention is used on a fixed-wing unmanned aerial vehicle, and is used to control the fixed-wing unmanned aerial vehicle to realize the switching between the forward flying state and the inverted flying state and the rapid adjustment of the flight direction through rolling and pitching. The UAV needs to be equipped with a multi-antenna satellite navigation and positioning system to ensure that the satellite navigation system can work normally during the maneuvering flight and to ensure the convergence of the inertial navigation system error. as attached figure 1 As shown, more than three satellite navigation antennas are evenly arranged on the head of th...

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Abstract

The invention provides a fixed-wing unmanned aerial vehicle rolling maneuvering control method. The method is applied to a fixed-wing unmanned aerial vehicle and provides an automatic control method for each control channel in the rolling maneuvering process. According to the method, 360-degree full-gesture seamless navigation is realized through a full-gesture combined navigation method; autonomous switching of the fixed-wing unmanned aerial vehicle between the upright flight state and the inverted flight state is realized through a rolling control method, and balance is rapidly established;and gravity potential energy is reasonably applied through a pitching rolling control method, safe and effective pitching rolling is realized, the flight direction of the unmanned aerial vehicle can be quickly changed under the condition that the safe angle of attack is guaranteed, and the unmanned aerial vehicle can be quickly separated from the dangerous situation in air combat. According to themethod, reasonable automatic control can be conducted on an engine and a control surface, flexible rolling maneuvering of the fixed-wing unmanned aerial vehicle can be realized, so that the unmannedaerial vehicle can freely switch between upright flying and inverted flying, and the flying direction can be quickly changed.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a field of simulating a fast maneuvering moving target by using a fixed-wing unmanned aerial vehicle, and belongs to the technical fields of unmanned aerial vehicles, autonomous navigation and flight control. Background technique [0002] The unmanned target drone is an important means of testing and identification of aviation weapon systems, and it is also an important support system for my country's actual combat military construction. Without a high-performance target drone, there will be no high-performance aviation weapon system. The U.S. Air Force launched the 5GAT fifth-generation stealth target aircraft project at a huge expense, providing a full-scale target aircraft that can simulate the real radar and infrared signal characteristics of stealth fighters for live ammunition shooting training and weapon testing. With the international service of stealth fighter je...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08
Inventor 赵文杰张媛媛
Owner ZHEJIANG UNIV
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