A rudderless aircraft attitude control mechanism

Abstract

The invention discloses a rudderless aircraft attitude control mechanism, specifically relates to the technical field of aircraft attitude control, comprising an aircraft, the lower surface of the aircraft is fixedly connected with the upper surface of the controller, the left side and the right side of the aircraft are The surfaces are respectively fixedly connected with the opposite surfaces of the four universal shells, the inner surfaces of the universal shells are provided with universal balls, and the upper surfaces of the universal balls are fixedly connected with the lower surface of the motor. The invention avoids the problem of complex operation and instability caused by the traditional use of slide rails and hinges in the wing to control the flight attitude, makes the control structure of the device simple and easy, and can maintain the rudder effect to achieve the optimal flight effect, and the device By automatically monitoring the state of the aircraft in real time, the purpose of automatically adjusting the flight attitude can be achieved for abnormal states, ensuring the accuracy of the heading, and further ensuring the intelligent control of the aircraft, which has good promotion value.

Description

technical field [0001] The invention relates to the technical field of aircraft attitude control, and more specifically, the invention relates to an attitude control mechanism for an aircraft without rudder surfaces. Background technique [0002] With the continuous development of aviation technology, aircraft are involved in various fields. For example, in the military, it can be used for reconnaissance and surveillance, communication relay, electronic countermeasures, etc. In civilian use, it can be used for geodesy, environmental monitoring, etc. In general, it can be used for atmospheric research, sampling and monitoring of nuclear, biological and chemical contaminated areas, etc. With the expansion of the application field of aircraft, people's demand for aircraft with simple structure and easy control is increasing. [0003] Most existing aircraft use conventional rudder surfaces to control the flight attitude of the aircraft, but when flying at high altitudes, the air...

AI Technical Summary

Problems solved by technology

[0004] In order to overcome the above-mentioned defects of the prior art, the present invention provides an attitude control mechanism for aircraft without rudder surfaces. The technical problem to be solved by the present invention is: the existing aircraft mostly use conventional rudder surfaces to control the flight attitude of the aircraft. When flying, the aircraft relies on the slide rails and hinges in the wings to control the flight attitude, resulting in a complex structure, and the rudder effect cannot achieve the optimal effect. In the prior art, in the process of controlling the flight of the aircraft, it is often necessary to hold the handle Perform position control and manually adjust when the flight of the aircraft deviates, which makes the operation more cumbersome

Images