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Flight control system for transportation aircraft

A technology of flight control system and aircraft, which is applied in the field of aircraft, can solve the problem of not having the normal operation ability of loading different materials, and achieve the effect of good adaptability and robustness

Active Publication Date: 2022-08-02
微至航空科技(北京)有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the existing large-scale fixed-wing UAVs are in the prototype demonstration stage. The experiments are carried out after sufficient simulation and verification of certain preset material transportation states that need to demonstrate flight, and they do not have normal operation to adapt to different material loading. ability

Method used

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  • Flight control system for transportation aircraft
  • Flight control system for transportation aircraft
  • Flight control system for transportation aircraft

Examples

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Embodiment Construction

[0080] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", " Orientation or position indicated by rear, left, right, vertical, horizontal, top, bottom, inside, outside, clockwise, counterclockwise, etc. The relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore It should not be construed as a limitation of the present invention.

[0081] In addition, the terms "first" and "second" are only used for descriptive purposes, and should not be construed as indicating or implying relative importance or implying the number of indicated technical...

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PUM

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Abstract

The invention provides a flight control system for a transport aircraft. The flight control system comprises control equipment, at least one intelligent container and a positioning base station, the position of the positioning base station is fixed; the intelligent container comprises a positioning module, a container processing module and a wireless communication module; the positioning module is used for determining a position; the container processing module is used for determining inertial data of the intelligent container; the control device is used for updating the current gravity center, weight and rotational inertia of the aircraft according to the inertia data of all the intelligent containers, the inertia data of the aircraft in the empty state and the inertia data of residual oil in the aircraft. According to the flight control system provided by the embodiment of the invention, the gravity center, the weight and the rotational inertia of the whole aircraft can be accurately updated in real time, good adaptability and robustness are achieved, the aircraft can be conveniently and accurately controlled subsequently based on the updated inertial data, and the flight control efficiency is improved. The safe flight of the aircraft in the article transportation and article air-drop process can be realized.

Description

technical field [0001] The present invention relates to the technical field of aircraft, in particular, to a flight control system for a transport aircraft. Background technique [0002] When the UAV carries out material transportation, its weight, center of gravity, moment of inertia, etc. vary with the loading, and there is a large deviation from the design point; when the UAV conducts material airdrops, its weight, center of gravity, moment of inertia, etc. There are jumps in loading and throwing. [0003] The current UAV flight control system does not pay sufficient attention and effectively deal with the weight, center of gravity, rotational inertia offset and jump that exist during material transportation and airdrop. Most of the existing large-scale fixed-wing UAVs are in the prototype demonstration stage. The experiments are carried out only after sufficient simulation verification is carried out for certain preset material transportation states that need to be demo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/25257
Inventor 林清张景
Owner 微至航空科技(北京)有限公司
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