Unmanned aerial vehicle flight control method, device, equipment and storage medium
By employing an architecture where the main process and hot standby process work together, the problem of data loss and loss of control in the event of a software crash in the UAV flight control system is solved. This achieves low-latency data recovery and stable flight control of the UAV, reduces the risk of performing disconnection actions, and does not increase hardware costs.
Patent Information
- Application Number
- CN202511817098.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-12-04
- Publication Date
- 2026-04-14
AI Technical Summary
Existing drone flight control systems cannot maintain data integrity when software crashes, leading to drone loss of control. Furthermore, existing solutions increase hardware costs or pose a risk of performing actions that cause the drone to lose connection.
An architecture is adopted in which the main process and the hot standby process work together. The hot standby process periodically monitors the survival status of the main process and retrieves and migrates backup data from shared memory to the restarted main process in case of an anomaly, ensuring the continuity of UAV flight control and data integrity.
It enables low-latency recovery of drones after software crashes, maintains the continuity of flight control, reduces the risk of performing disconnection maneuvers, and does not increase hardware costs.