Semi-object guidance simulation method and system

A simulation method and simulation system technology are applied in the field of semi-physical guidance simulation methods and simulation systems to achieve the effects of improving accuracy and reducing errors

Active Publication Date: 2017-05-17
BEIJING RUNKE GENERAL TECH
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  • Claims
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Problems solved by technology

[0004] But for non-active homing guidance systems, there is a lack of hardware-in-the-loop guidance simulation methods and simulation systems that can perform complete functional and performance tests on them in the prior art

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  • Semi-object guidance simulation method and system
  • Semi-object guidance simulation method and system
  • Semi-object guidance simulation method and system

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Embodiment Construction

[0048] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0049] An embodiment of the present invention provides a hardware-in-the-loop guidance simulation method, which is applied to a hardware-in-the-loop guidance simulation system including a guidance station, a guidance system, an aircraft control system, an aircraft simulator, a multi-degree-of-freedom motion simulation platform, and a motion simulation control system; Such as figure 2 As shown, the hardware-in-the-loop guidance simulation method includes:

[...

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Abstract

The invention discloses a semi-object guidance simulation method and system. The method comprises that an aiming device of a guidance station is placed in two axes of a multi-freedom movement simulation platform; an aircraft simulator is placed in two random axes, except the two axes for placing the aiming device, of the multi-freedom movement simulation platform; a movement simulation control system controls angular movement of the aiming device in two directions and angular movement of the aircraft simulator in two directions; the aiming device is used to observe the aircraft simulator to obtain angular information of an aircraft; and according to the obtained aircraft angular information, input target angular information and a three-point guidance relation equation, a control instruction is output to an aircraft control system. The semi-object guidance simulation method realizes simulation of a guidance process and a non-active homing guidance system.

Description

technical field [0001] The invention relates to the field of hardware-in-the-loop simulation technology, more specifically, to a simulation method and simulation system for hardware-in-the-loop guidance. Background technique [0002] The application fields of the guidance system mainly include missile target guidance, satellite launch, unmanned aerial vehicle flight, and aircraft systems to achieve different mission requirements. The definition of guidance is the technology and method of guiding and controlling the aircraft to fly to the target or predetermined orbit according to certain rules. The guidance system mainly includes the guidance system, the aircraft and the aircraft control system. The working process is that the guidance system continuously measures the relative positional relationship between the aircraft and the target or the predetermined orbit, sends out guidance information, and transmits it to the aircraft control system to control the flight of the airc...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 罗喜霜谢竹峰郑亮
Owner BEIJING RUNKE GENERAL TECH
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