Aircraft control system
By working together with the attitude detection device and the control module, the problem of the aircraft drifting due to airflow was solved, and the nose was automatically corrected to align with the direction of the incoming flow, thus improving the stability and accuracy of the aircraft.
WO2026144987A1PCT designated stage Publication Date: 2026-07-09AUTOFLIGHT (KUNSHAN) CO LTD
Patent Information
- Authority / Receiving Office
- WO · WO
- Patent Type
- Applications
- Current Assignee / Owner
- AUTOFLIGHT (KUNSHAN) CO LTD
- Filing Date
- 2025-12-16
- Publication Date
- 2026-07-09
Smart Images
Figure CN2025142927_09072026_PF_FP_ABST
Abstract
The present invention relates to the field of aircrafts. Disclosed is an aircraft control system, for use in controlling an aircraft to automatically align with an oncoming flow direction. Flight modes include a vertical take-off and landing mode, a cruise mode, and a transition mode. The control system comprises a flight control module and a control module. The control module comprises a user-operable control device. The control device may send different instructions to the flight control module, for controlling the aircraft to automatically align with the oncoming flow direction.
Need to check novelty before this filing date? Find Prior Art