An aircraft control system

CN122308335APending Publication Date: 2026-06-30AUTOFLIGHT (KUNSHAN) CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
AUTOFLIGHT (KUNSHAN) CO LTD
Filing Date
2024-12-30
Publication Date
2026-06-30

AI Technical Summary

Technical Problem

Aircraft are easily affected by airflow during flight, causing them to deviate. Existing technology makes it difficult to automatically correct their position to align with the direction of the airflow.

Method used

The attitude detection device (such as a gyroscope, accelerometer or magnetometer) is used to detect changes in the aircraft's attitude, and the control module controls the aircraft to automatically correct its attitude, including the correction of roll angle, yaw angle and pitch angle. The control device sends commands to make the aircraft's nose align with the oncoming wind direction.

Benefits of technology

It enables the aircraft to automatically correct its position after deviating, ensuring that the nose is aligned with the direction of the incoming flow, thus improving flight stability and accuracy.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN122308335A_ABST
    Figure CN122308335A_ABST
Patent Text Reader

Abstract

This invention belongs to the field of aircraft and discloses an aircraft control system for controlling an aircraft to automatically align with the incoming wind direction. The flight modes include vertical takeoff and landing mode, cruise mode, and switching mode. The control system includes a flight control module and a control module. The control module includes a control device that can be operated by the user. The control device can send different commands to the flight control module to control the aircraft to automatically align with the incoming wind direction.
Need to check novelty before this filing date? Find Prior Art