Unmanned aerial vehicle flight simulation method and system

A flight simulation and UAV technology, applied in the field of flight simulation, can solve the problem of high cost, achieve comprehensive and reliable results, reduce economic costs and time costs, and save time and energy.

Pending Publication Date: 2021-03-30
GENERAL ENG RES INST CHINA ACAD OF ENG PHYSICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] like figure 1 As shown, the common practice of UAV flight simulation is to realize the three-axis turntable in the laboratory. The output command is connected to the simulation computer. After the simulation computer receives the instructions of each actuator, it runs the dynamic model of the UAV in real time and calculates the status information (position, speed, acceleration, etc.) of the UAV. The fixed data format transmits the data to the flight control system, and at the same time drives the movement of the turntable so that the flight control system can perceive the angular velocity informat

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  • Unmanned aerial vehicle flight simulation method and system

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[0023]In order to make the objects, technical solutions, and advantages of the present invention more clear, the technical solutions in the embodiments in the embodiments will be described in contemplation in the accompanying drawings in the embodiment of the present invention. Obviously, the described embodiments are all embodiments of the invention, not all of the embodiments. Components of the embodiments of the present invention described and illustrated in the drawings herein can be arranged and designed in various configurations.

[0024]Thus, the following detailed description of the embodiments of the invention as provided in the drawings are not intended to limit the scope of the invention, but only the selected embodiments of the present invention are shown. Based on the embodiments of the present invention, those of ordinary skill in the art will belong to the scope of the present invention without all other embodiments obtained without creative labor.

[0025]It should be note...

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Abstract

The invention discloses an unmanned aerial vehicle flight simulation method and system, and relates to the field of flight simulation. The method comprises the steps of: S1, importing initial data into a ground station and transmitting the data to an unmanned aerial vehicle; S2, acquiring an execution mechanism output instruction according to a simulated flight state parameter and a flight plan, and transmitting the execution mechanism output instruction and periodic telemetry data to the ground station; S3, outputting and displaying periodic telemetry data in real time by the ground station,acquiring a next simulated flight state parameter according to the simulated flight state parameter, the execution mechanism output instruction and an unmanned aerial vehicle kinetic model, transmitting the next simulated flight state parameter to the unmanned aerial vehicle, and entering S2; the system comprises a data input module, a simulation module, a flight control system and a display module. The ground station has the dynamic simulation calculation capability, the unmanned aerial vehicle can perform flight mode switching, and the ground station can send the flight state of the unmannedaerial vehicle in real time, so that the simulated flight test can be completed without a three-axis turntable, clamps and cables do not need to be customized, and the economic and time costs are reduced; the whole "simulated flight" is simplified, and the time and energy of personnel are saved.

Description

technical field [0001] The invention relates to the field of flight simulation, in particular to a flight simulation method and system for an unmanned aerial vehicle. Background technique [0002] Such as figure 1 As shown, the common practice of UAV flight simulation is to realize the three-axis turntable in the laboratory. The output command is connected to the simulation computer. After the simulation computer receives the instructions of each actuator, it runs the dynamic model of the UAV in real time and calculates the status information (position, speed, acceleration, etc.) of the UAV. The fixed data format transmits the data to the flight control system, and at the same time drives the movement of the turntable so that the flight control system can perceive the angular velocity information in real time. After receiving all the information, the flight control system can calculate the required control in real time according to the mission instructions and control laws....

Claims

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Application Information

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IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 邓坤黄佳陈强洪袁鸣周欢
Owner GENERAL ENG RES INST CHINA ACAD OF ENG PHYSICS
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