Parallel computation and distribution control method for flight simulation system
Patent Information
- Authority / Receiving Office
- CN · China
- Current Assignee / Owner
- 冯岩
- Publication Date
- 2015-05-06
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to the technical field of flight simulation, and more specifically, relates to a parallel computing and distributed control method for a flight simulation system. Background technique
[0002] The flight simulation system is mainly used in flight training and related engineering design and research fields. Based on control theory, aviation technology, computer technology, precision machinery manufacturing technology, etc., it integrates various software and hardware systems to truly restore the aircraft in flight and The effect in the ground state simulates the state, environment and conditions of the mission process, and provides the pilot with similar visual, auditory, kinematic and control sensations. The core of the flight simulation system is the flight simulation model, including the aerodynamic model, external environment model, aircraft system model, avionics system model, etc. In addition to the flight simulation model, t...