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A Portable Ground Online Flight Simulation System

A flight simulation and portable technology, applied in the field of computer simulation, can solve the problems of long cycle, incomplete inspection of UAV system status, and poor economy.

Active Publication Date: 2021-04-27
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, semi-physical simulation tests driven by mathematical models cannot effectively simulate the collaborative work response of UAV avionics, electromechanical, flight control, and power systems after cross-linking. Recurrence, the state of the UAV system cannot be fully inspected. For this reason, some research and development units have built an iron bird test bed that is consistent with the real airborne environment to test the state of the UAV system, but the equipment state of the Iron Bird test bed cannot It is always guaranteed to be consistent with the state of the airborne equipment, and the cost of building an iron bird test bed is too high, the economy is not good, the cycle is long, and it is not mobile

Method used

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  • A Portable Ground Online Flight Simulation System
  • A Portable Ground Online Flight Simulation System
  • A Portable Ground Online Flight Simulation System

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0025] Such as figure 1 As shown, a portable ground online flight simulation system includes a console computer 1, a simulation computer 2, a hub 3 and an airborne device 4, the console computer 1 is connected to the simulation computer 2 through Ethernet, and the hub 3 is connected to the simulation computer 2 through The cables are respectively connected with the simulation computer 2 and the airborne equipment 4, and the console computer 1 is a high-performance PC, which is used for simulation process control, simulation data display, simulation data display record, and initial parameter setting of the unmanned aerial vehicle , wind field environment injection and fault model injection, the simulation computer 2 is an embedded computer, used for real-time solving of unmanned aerial vehicle mathematical model, sensor real-time simulation, wind field model solving, fault model solving, physical and electrical Interface simulation, the hub 3 is used to distribute the electrica...

Embodiment 2

[0028] Such as figure 1As shown, a portable ground online flight simulation system includes a console computer 1, a simulation computer 2, a hub 3 and an airborne device 4, the console computer 1 is connected to the simulation computer 2 through Ethernet, and the hub 3 is connected to the simulation computer 2 through The cables are respectively connected with the simulation computer 2 and the airborne equipment 4, and the console computer 1 is a high-performance PC, which is used for simulation process control, simulation data display, simulation data display record, and initial parameter setting of the unmanned aerial vehicle , wind field environment injection and fault model injection, the simulation computer 2 is an embedded computer, used for real-time solving of unmanned aerial vehicle mathematical model, sensor real-time simulation, wind field model solving, fault model solving, physical and electrical Interface simulation, the hub 3 is used to distribute the electrical...

Embodiment 3

[0037] Such as figure 1 As shown, a portable ground online flight simulation system includes a console computer 1, a simulation computer 2, a hub 3 and an airborne device 4, the console computer 1 is connected to the simulation computer 2 through Ethernet, and the hub 3 is connected to the simulation computer 2 through The cables are respectively connected with the simulation computer 2 and the airborne equipment 4, and the console computer 1 is a high-performance PC, which is used for simulation process control, simulation data display, simulation data display record, and initial parameter setting of the unmanned aerial vehicle , wind field environment injection and fault model injection, the simulation computer 2 is an embedded computer, used for real-time solving of unmanned aerial vehicle mathematical model, sensor real-time simulation, wind field model solving, fault model solving, physical and electrical Interface simulation, the hub 3 is used to distribute the electrica...

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PUM

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Abstract

The invention discloses a portable ground online flight simulation system, which includes a console computer, a simulation computer, a hub and an airborne device. The console computer is connected to the simulation computer through an Ethernet, and the hub is respectively connected to the simulation computer and the simulation computer through cables. Airborne equipment connection, the console computer is a high-performance PC, used for simulation process control, simulation data display, simulation data display record, UAV initial parameter setting, wind field environment injection and fault model injection, The simulation computer is an embedded computer, which is used for real-time solving of the unmanned aerial vehicle mathematical model, real-time simulation of sensors, wind field model solving, fault model solving, physical electrical interface simulation, and the hub is used for the simulation computer Distribution of electrical connections with onboard equipment. The invention checks the UAV system in an efficient, safe, economical and comprehensive manner, ensures the flight safety of the UAV, comprehensively verifies the correctness and rationality of the UAV system, and provides pilots with UAV system information without building The iron bird test bench is low in cost, good in economy, short in cycle, small in size and easy to move.

Description

technical field [0001] The invention belongs to the technical field of computer simulation, in particular to a portable ground online flight simulation system. Background technique [0002] In today's world, with the continuous improvement of aircraft autonomy and intelligence, drones are more and more frequently used for battlefield reconnaissance, monitoring and attack tasks, and have gradually become an indispensable and efficient aviation weapon in warfare. In order to save development costs, speed up development, and reduce flight test risks, it is necessary to carry out necessary simulation tests to ensure the safety of UAV flight. [0003] At present, research and development units at home and abroad mainly use semi-physical simulation tests to verify the correctness of airborne software. However, semi-physical simulation tests driven by mathematical models cannot effectively simulate the collaborative work response of UAV avionics, electromechanical, flight control,...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 熊洪睿余长贵田凯黄捷李何瑜张文统
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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