Aircraft control method and aircraft controlled therewith

A control method and aircraft technology, applied in the field of aircraft, can solve problems such as lack of long-term endurance, need for runways, lack of vertical take-off and landing, etc.

Active Publication Date: 2017-12-26
CHENGDU FANGZHOU INTELLIGENT CONTROL TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Fixed-wing aircraft use wings to generate lift, need a runway, and do not have the ability to take off and land vertically; rotor-type aircraft have the ability to take off and land vertically, but do not have long-term endurance and the ability to float with the help of wings

Method used

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  • Aircraft control method and aircraft controlled therewith

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Embodiment

[0042] Such as figure 1 As shown, an aircraft includes a fuselage 1, a nose 11, a left wing 2, a right wing 3, a control system, a left rudder surface 4, a right rudder surface 5, a left motor 6, a right motor 7, a left vertical tail 8 and a right vertical tail. Tail 9. The two sides of the fuselage are respectively provided with a left wing and a right wing which can glide by means of airflow during level flight, and the bottom of the left wing and the right wing is provided with a left rudder surface and a right rudder surface which can adjust the activity angle, and the bottom of the left wing and the right wing are also respectively A left vertical empennage and a right vertical empennage as a landing gear are provided; a left motor and a right motor equipped with propellers are respectively arranged on the left wing and the right wing. The output end of the control system is connected with the left motor, the right motor, the left rudder surface and the right rudder surf...

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Abstract

The invention discloses an aircraft control method and the aircraft controlled therefor, which solves the shortcomings of fixed-wing aircraft and rotary-wing aircraft in the prior art. Aircraft, including fuselage, nose, left wing, right wing, control system, left rudder surface, right rudder surface, left motor, right motor, left vertical tail and right vertical tail. The two sides of the fuselage are respectively provided with a left wing and a right wing which can glide by means of airflow during level flight, and the bottom of the left wing and the right wing is provided with a left rudder surface and a right rudder surface which can adjust the activity angle, and the bottom of the left wing and the right wing are also respectively A left vertical empennage and a right vertical empennage as a landing gear are provided; a left motor and a right motor equipped with propellers are respectively arranged on the left wing and the right wing. The output end of the control system is connected with the left motor, the right motor, the left rudder surface and the right rudder surface, and the control system includes a processor, a gyroscope and an accelerometer connected with the processor. Through the above technical solution, the problems in the prior art can be well solved.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an aircraft control method and an aircraft controlled therefor. Background technique [0002] With the development of science and technology, the technology of unmanned aerial vehicles is becoming more and more advanced. There are mainly two types of unmanned aerial vehicles on the market, namely fixed-wing aircraft and rotary-wing aircraft. Due to structural limitations, fixed-wing aircraft and rotary-wing aircraft each have their advantages and disadvantages. Fixed-wing aircraft use wings to generate lift, need a runway, and do not have the ability to take off and land vertically; rotor-type aircraft have the ability to take off and land vertically, but do not have long-term endurance and the ability to float with the help of wings. Contents of the invention [0003] The object of the present invention is to overcome the defects of the prior art, and provide a control metho...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/22B64C9/00B64C19/00B64D27/24B64D31/00G05D1/08
CPCG05D1/0808G05D1/0858B64C9/00B64C19/00B64C27/22B64D27/24B64D31/00B64U10/00B64U2201/10B64U50/19
Inventor 孙宇舟
Owner CHENGDU FANGZHOU INTELLIGENT CONTROL TECH CO LTD
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