Unmanned aerial vehicle semi-physical simulation system

A technology of physical simulation and simulation system, which is applied in the field of semi-physical simulation system of unmanned aerial vehicles, can solve the problems that the operating environment of the measured object deviates from the actual operating environment, the test function is single, and the real-time performance is low, so as to increase scalability and versatility sexual effect

Inactive Publication Date: 2021-12-24
XIAN LINGKONG ELECTRONICS TECH CO LTD
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AI Technical Summary

Problems solved by technology

As one of the key modules in the research and development of the UAV flight control system, the semi-physical simulation platform provides an efficient and extremely small error comprehensive UAV semi-physical simulation platform for the design of flight control algorithms through flight simulation; most of the semi-physical simulation The system has the following problems: low real-time performance, the operating environment of the tested object deviates from the actual operating environment; the test function is single; the test results cannot be intuitively reflected

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  • Unmanned aerial vehicle semi-physical simulation system
  • Unmanned aerial vehicle semi-physical simulation system
  • Unmanned aerial vehicle semi-physical simulation system

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Embodiment Construction

[0026] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0027] A semi-physical simulation system for unmanned aerial vehicles in the present invention includes a test management system, an IO simulation system, a simulation computing system, a signal conditioning unit, a signal disconnection system, a fault injection system and a flight control computer, such as figure 1 and Figure 4 Shown:

[0028] The simulation management system of the present invention transmits simulation scheduling and simulation parameters to the simulation computing system, and the simulation computing system feeds back the simulation status and simulation data to the simulation management system, that is, completes the comprehensive management of the simulation environment; the simulation computing system transmits the model excitation data to IO simulation system, the IO simulation system feeds back the feedback data o...

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Abstract

The invention discloses an unmanned aerial vehicle semi-physical simulation system, which comprises a test management system, a simulation calculation system, an IO simulation system, a signal conditioning unit, a signal disconnection system, a fault injection system and a flight control machine object, and is matched with a semi-physical simulation system for resolving an environment in real time. The excitation signal of a tested object can be closer to the electrical signal of the real operation environment, and the feedback signal of the tested object can be obtained in time, so that the semi-physical simulation test is closer to the real test environment; an airborne equipment model is isolated from an IO scheduling model calculation environment, so that the operation resource of an airborne equipment mathematical model can be isolated from an equipment IO scheduling resource, and the calculation real-time performance of a dynamic model and the airborne equipment model is more powerfully guaranteed; and a signal conditioning and disconnecting device increases expandability and universality for the semi-physical simulation system, and the fault injection device provides environment support for a fault tolerance test of a tested object in a simulation test.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle simulation, and relates to a semi-physical simulation system for an unmanned aerial vehicle. Background technique [0002] As the control center and control algorithm operation system of the UAV, the flight control computer mainly completes the functions of flight state management and control command resolution. Due to its unmanned nature, there are higher performance requirements in terms of remote communication and control algorithm reliability and stability. The verification test of the flight control computer becomes an important part of the UAV reliability test. Therefore, in order to successfully complete the pre-design of the unmanned aerial vehicle, providing a complete and reliable flight simulation platform for the development of the flight computer onboard code is directly related to the efficiency and success of the entire research and development iteration process. A...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 王华杨海东郭宏选
Owner XIAN LINGKONG ELECTRONICS TECH CO LTD
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