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A flight control method and system based on complex low altitude

A flight control, low-altitude technology, applied in general control systems, control/regulation systems, attitude control, etc., and can solve problems such as less research on flight control

Active Publication Date: 2020-09-08
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Few researches on complex low-altitude flight control

Method used

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  • A flight control method and system based on complex low altitude
  • A flight control method and system based on complex low altitude
  • A flight control method and system based on complex low altitude

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Embodiment Construction

[0077] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0078] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0079] figure 1 It is a schematic flow chart of the flight control method based on complex low altitude in the present invention. Such as figure 1 As shown, the control method includes:

[0080] Step 100: Obtai...

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Abstract

The invention discloses a flight control method and a flight control system on the basis of complicated low altitudes. The flight control method includes acquiring environmental information in set threshold ranges around to-be-controlled aircrafts; acquiring flight plans of the to-be-controlled aircrafts; judging whether conflict between the environmental information and the flight plans of the to-be-controlled aircrafts exists or not, and allowing the to-be-controlled aircrafts to fly according to the flight plans if the conflict does not exist; acquiring conflict information of the environmental information and the flight plans if the conflict exists; adjusting the flight plans according to the conflict information to obtain adjusted flight plans and allowing the to-be-controlled aircrafts to fly according to the adjusted flight plans. The environmental information includes information of other aircrafts, weather information and topographic information. The flight plans comprise flight routes, flight heights and flight speeds which correspond to a plurality of legs. The flight control method and the flight control system have the advantage that control and simulation analysis canbe carried out on flight at the complicated low altitudes by the aid of the flight control method and the flight control system which is a simulation system.

Description

technical field [0001] The invention relates to the field of air traffic, in particular to a complex low-altitude flight control method and system. Background technique [0002] Low-altitude airspace is an important part of my country's airspace system, which contains great economic and social value. With the increasing demand for low-altitude flights, making full use of low-altitude resources and scientifically controlling low-altitude flights has become an important issue facing the world's aviation powers. Complex low-altitude generally refers to the busy low-altitude airspace where controlled and uncontrolled airspace is coupled to operate, affected by complex terrain, and mixed with various types of general aircraft. The complex low-altitude flight situation refers to the overall flight state and development trend formed by the interaction of dense flight groups, various influencing behaviors, and airspace environment in a certain space-time, which can reflect the spac...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10G05D1/08G05B17/02
CPCG05B17/02G05D1/0808G05D1/101
Inventor 张洪海江程鹏邱启伦黄晶晶钱晓鹏
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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