Simulation method of atmospheric turbulence on flight simulator
A technology of flight simulator and simulation method, which is applied to simulation devices, simulators, instruments, etc. of space navigation conditions, can solve the problems of poor simulation accuracy and fidelity, and achieve the goal of improving simulation fidelity, avoiding errors and distortions, Accurate and realistic effect
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2010-12-29
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention belongs to the field of flight simulation. The invention discloses a method for simulating atmospheric turbulence on a flight simulator, which is used for improving the simulation accuracy of the flight performance and flight quality of the flight simulator, and relates to the fields of flight systems, motion systems and instrument systems of the flight simulator. Background technique
[0002] Atmospheric turbulence has an important impact on aircraft flight performance, especially flight safety. Therefore, how to establish a mathematical model that can accurately simulate atmospheric turbulence and implement it on a flight simulator is an urgent problem to be solved. In the simulation of turbulent flow, a big technical problem is the simulation of the buffeting of the aircraft on the corresponding degrees of freedom (including the buffeting of the instrument indication and the buffeting of the moving platform) brought about by the atmos...
Examples
Embodiment Construction
[0019] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
[0020] Start the turbulent flow program on the main computing computer 1, the random number is generated from the signal, after the rationalization of the spectral functions of the turbulent flow components in the three directions, and then processed by the filter, the three components of the turbulent flow are formed, and the These three turbulence components are added to the flight speed of the aircraft through coordinate transformation, and then substituted into the motion equation for settlement, and finally the relevant aircraft flight state parameters are obtained (see figure 1 , 4 ).
[0021] according to figure 2 , image 3 , Figure 4 , output the flight state parameters sent to the motion system to the network card 2, then to the HUB 3, and then to the network card 4, and then output to the platform control computer 5 through the network ...