Virtual automatic flight control interface human-computer interaction system and method

By designing a virtual automatic flight control interface on the integrated display and control subsystem of the aircraft cockpit, the problem of high failure rate of traditional automatic flight control boards is solved, a backup function is realized in case of failure, the reliability and ease of operation of the automatic flight control system are improved, and the needs of modern flight missions are met.

CN119472619BActive Publication Date: 2026-03-17SHAANXI AIRCRAFT CORPORATION
3 Cites 0 Cited by

Patent Information

Application Number
CN202411490987.X
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-10-24
Publication Date
2026-03-17
Estimated Expiration
2044-10-24

AI Technical Summary

Technical Problem

Traditional automatic flight control boards have a high failure rate, resulting in low mission reliability and making it difficult to meet the requirements of modern aircraft for long-endurance and multi-scenario missions.

Method used

Design a virtual automatic flight control interface human-machine interaction system. By residing a virtual interface on the multi-functional display of the cockpit integrated display and control subsystem, data interconnection is achieved through a bus network, providing backup automatic flight control functions, including mode/mode selection, numerical loading and display, and switching to the virtual interface to continue the flight mission in case of failure.

Benefits of technology

It improves the mission reliability of the automatic flight control subsystem, provides a convenient way to select autopilot functions, ensures that pilots can continue to perform flight missions when the automatic flight control board fails, and meets the mission requirements of long flight time and multiple scenarios.

✦ Generated by Eureka AI based on patent content.
Patent Text Reader

Abstract

The present application belongs to the field of automatic flight control, and particularly relates to a virtual automatic flight control interface human-computer interaction system and method. The system comprises: a cockpit integrated display control subsystem, a plurality of instruction solving units, an automatic flight control board, a cockpit integrated display control subsystem, a power control device, the cockpit integrated display control subsystem comprises a digital keyboard and a multifunctional display, the automatic flight control board is crosslinked with the instruction solving units and the power control device through an HB6096 bus, a virtual interface is resident on the multifunctional display of the cockpit integrated display control subsystem, the multifunctional display is crosslinked with the instruction solving units through an AFDX network bus, the multifunctional display is crosslinked with the power control device through the HB6096 bus, the instruction solving units are crosslinked with a central warning system through the AFDX network bus, and the digital keyboard of the cockpit integrated display control system is connected with the multifunctional display through a system internal bus and used for sending a target value and the like signal to the multifunctional display.
Need to check novelty before this filing date? Find Prior Art