Low-altitude aircraft engineering simulation system

By designing a low-altitude aircraft engineering simulation system, data is collected using the central control stick and auxiliary control stick, and the flight control software is optimized. This solves the problems of poor adaptability and complex optimization iteration of low-altitude aircraft simulators, and achieves more efficient pilot operation adaptation and aircraft response.

CN121565041APending Publication Date: 2026-02-24上海沃兰特航空科技股份有限公司
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Patent Information

Application Number
CN202610013521.3
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2026-01-06
Publication Date
2026-02-24

AI Technical Summary

Technical Problem

Existing low-altitude aircraft engineering simulators are mostly modified from simulators for fixed-wing large aircraft, which cannot fully adapt to the needs of low-altitude aircraft. This leads to differences in the experience of pilots, and the optimization and iteration process of flight control software is complex, resulting in low efficiency in verifying the optimization effect.

Method used

A low-altitude aircraft engineering simulation system was designed, including a cockpit, a simulator server, and a host computer. Operational data is collected through a central control stick and an auxiliary control stick. Control commands are output using the simulator server, and the host computer optimizes the flight control software to adapt to the pilot's operating habits and optimize the flight process.

Benefits of technology

It effectively reduces the sense of difference for pilots during low-altitude aircraft simulation flight, improves the optimization efficiency and adaptability of flight control software, and enhances the pilot's operating experience and the aircraft's response performance.

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Abstract

The invention relates to an engineering simulation system for a low-altitude aircraft. The engineering simulation system comprises an engineering simulator of the low-altitude aircraft, a simulator server and an upper computer, the engineering simulator comprises a cockpit; the cockpit comprises a driving seat, a central control column and an auxiliary control column; the central control stick is used for simulating accelerator operation and yaw operation of the low-altitude aircraft; the auxiliary joystick is used for simulating pitching operation and rolling operation of the low-altitude aircraft; sensors are respectively arranged in the central steering column and the auxiliary steering column, and are used for collecting operation data generated when a pilot operates the steering column; the simulator server receives the operation data and outputs a control instruction corresponding to the operation data; the upper computer receives the operation data and flight data corresponding to the flight process, and the operation data and the flight data are used for optimizing the simulator server. Therefore, the difference feeling in the process that a pilot uses the low-altitude aircraft engineering simulator to carry out simulation flight can be effectively reduced.
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