A method for controlling the automatic leveling of an aircraft

A control method and aircraft technology, applied in the field of aviation flight control, can solve problems such as long leveling time and large load and overload, and achieve the effect of simple design, strong usability and typical structure

Active Publication Date: 2019-04-23
SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide an automatic leveling control method of an aircraft to solve the problems of excessive overload and long leveling time in the existing automatic leveling control method of an aircraft

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  • A method for controlling the automatic leveling of an aircraft
  • A method for controlling the automatic leveling of an aircraft
  • A method for controlling the automatic leveling of an aircraft

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Embodiment Construction

[0018] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention relates to the technical field of aviation flight and particularly relates to an automatic level-off control method of an airplane, aiming at solving the problems of an existing automatic level-off control method of the airplane that the load is too great and the level-off time is long. The automatic level-off control method of the airplane comprises the following steps: dividing an included angle between a pitch angle initial position of the airplane at a flying state and the horizontal plane into a plurality of pre-set intervals; and setting level-off manners for controlling the airplane in the different ranges respectively so as to automatically carry out automatic level-off according to the level-off manner matched with the interval of the pitch angle of the airplane under an automatic level-off manipulation mode. The automatic level-off control method of the airplane has a simple design and a typical structure, and has a relatively strong utilization capability and a wide application range; and the airplane can enter a level-off mode from any space position, and a level-off control flow meets a pilot operation method.

Description

technical field [0001] The invention relates to the technical field of aviation flight control, in particular to an aircraft automatic leveling control method. Background technique [0002] Automatic leveling function is a very important function of the automatic flight control system of the aircraft. The function of the automatic leveling mode is that when the pilot loses the spatial position, turning on the leveling mode can guide the aircraft from any spatial position to the level. [0003] However, in the current aircraft design, the design of the leveling function of the aircraft is relatively simple, and the automatic leveling cannot be performed at all angles. If the load is too large, it will take a long time to level off. Contents of the invention [0004] The object of the present invention is to provide an aircraft automatic leveling control method to solve the problems of excessive load and overload and long leveling time of the existing aircraft automatic le...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08
CPCG05D1/0808
Inventor 丁岩王志刚张秀林桂敬玲曲晓雷
Owner SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP OF CHINA
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