An intelligent flight control system for manned aircraft

A flight control system and aircraft technology, applied in aircraft control, aircraft parts, aircraft black boxes, etc., can solve the problems of safety and reliability that cannot meet the needs of manned automatic flight, aircraft acquisition functions, etc.

Active Publication Date: 2022-06-07
广东海鸥飞行汽车集团有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, these flight control systems are mainly for remote control flight or preset path flight, and have less functions for collecting the state of the aircraft itself, and cannot meet the requirements of manned automatic flight in terms of safety and reliability.

Method used

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  • An intelligent flight control system for manned aircraft
  • An intelligent flight control system for manned aircraft
  • An intelligent flight control system for manned aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0042]Example 1, as figure 1 As shown, an intelligent flight control system for a manned aircraft includes a flight control system host 1, a GPS and an external magnet module 2, a multi-channel PWM output control module 3, a digital radio station and an antenna 4, a black box 5, and a Beidoutian communication module. And antenna 6, information acquisition module A 7, information collector B 8, RS232 / RS422 reserved input and output interface 9, artificial intelligence platform 11 and flight environment perception system 10, GPS and external magnet module 2, multi-channel PWM output Control module 3, digital radio station and antenna 4, black box 5, Beidoutian communication module and antenna 6, information acquisition module A 7, information collector B 8, RS232 / RS422 reserved input and output interface 9, artificial intelligence platform 11 and The flight environment perception system 10 is connected to the mainframe 1 of the flight control system to realize the collection and...

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PUM

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Abstract

This application discloses an intelligent flight control system for manned aircraft, including a flight control system host, GPS and external magnet modules, multi-channel PWM output control modules, digital transmission stations and antennas, black boxes, Beidoutian communication modules and antennas, information Acquisition module A, information acquisition device B, RS232 / RS422 reserved input and output interface, artificial intelligence platform and flight environment perception system, GPS and external magnet module, multi-channel PWM output control module, digital radio station and antenna, black box, Beidoutian communication module and antenna, information collection module A, information collection device B, RS232 / RS422 reserved input and output interfaces, artificial intelligence platform and flight environment perception system are connected to the flight control system host. The invention has the following advantages: the acquisition and monitoring of the flight state of the manned aircraft is realized, and the power system of the manned aircraft is controlled for reliable flight by autonomous planning or according to the flight mode / route set by the user.

Description

technical field [0001] The invention relates to an intelligent flight control system for a manned aircraft, which belongs to the technical field of data identification and processing of manned aircraft. Background technique [0002] Thanks to the increasing maturity of manned aircraft, manned aircraft is gradually entering the daily life of the public, and air travel is no longer out of reach. Manned aircraft are developing in the direction of vertical take-off and landing, large load, long endurance, etc., but their safety and reliability are the ultimate goals of manned aircraft. [0003] As the flight brain of the manned aircraft, the flight control system directly determines the safety of the manned aircraft. Therefore, how to improve the safety and reliability of the flight control system is an important issue in the development of the manned aircraft. [0004] Most of the existing flight control systems are the flight control systems of small unmanned aerial vehicles ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C19/00B64D45/00
CPCB64C19/00B64D45/00B64D2045/0065B64D2045/0085
Inventor 颜军董文岳杨革黄小虎李光冯晓
Owner 广东海鸥飞行汽车集团有限公司
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