Injection-type semi-physical simulation system for laser-guided missile

A half-in-the-loop simulation and laser-guided technology, applied in the field of injection-type half-in-the-loop simulation system, can solve the problems of high cost and large experimental site, and achieve the effect of reducing costs

Inactive Publication Date: 2016-03-23
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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Problems solved by technology

[0004] In order to solve the problem that the experimental field is relatively large and the cost is high in the semi-physical simulation system based on projection diffuse reflection, the present invention proposes an injection-type semi-physical simulation system for laser-guided missiles

Method used

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  • Injection-type semi-physical simulation system for laser-guided missile
  • Injection-type semi-physical simulation system for laser-guided missile

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Embodiment Construction

[0018] The present invention will be described in further detail below in conjunction with the accompanying drawings.

[0019] like figure 1 As shown, the hardware-in-the-loop simulation system of the present invention mainly includes a simulation platform, a seeker, a GNC system, a target simulation device, an attitude simulation device, an acceleration simulation device, a steering gear, and a load simulation device. Among them, the simulation platform solves the projectile model and target model. The simulation platform obtains the attitude angle and acceleration of the missile by solving the missile model, which are used to control the motion of the attitude simulation device and the output of the acceleration simulation device respectively. The simulation platform obtains the line-of-sight angle by solving the target model, which is used to control the movement of the target simulation device. The seeker receives the laser beam generated by the target simulation device,...

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Abstract

The invention provides an injection-type semi-physical simulation system for a laser-guided missile, and belongs to the technical field of laser-guided missile development. In order to overcome the projection diffuse reflection type defect, the system comprises a simulation platform, a missile guider, a guidance, navigation and control (GNC) system, a target simulation device, a posture simulation device, an acceleration simulation device, a load simulation device and a launch-control device. The simulation platform mainly undertakes building and calculating of all mathematical models and is communicated with other equipment participating in simulation. The missile guider receives a laser signal sent from the target simulation device to form light spot gravity center location information, and a target orientation is supplied to the GNC system through a control area network (CAN) bus network. The GNC system is installed on the posture simulation device. Light emitting from the target simulation device is injected into the missile guider to simulate target movement. The posture of the missile is simulated through the posture simulation device, and the angular motion characteristics of the missile in the air are reproduced. Output of an accelerometer is simulated through the acceleration simulation device. The load simulation device is used for simulating the aerodynamic moment on a steering engine in the flying process of the missile. The launch-control device mainly completes self-checking and confirming of equipment, data loading and launching instructions on the missile.

Description

technical field [0001] The invention relates to an injection-type semi-physical simulation system for developing a small laser-guided missile, belonging to the technical field of laser-guided missile development. Background technique [0002] Semi-physical simulation refers to the simulation of inserting part of the physical object into the simulation loop of the system. Hardware-in-the-loop simulation can improve the authenticity of guided weapon simulation experiments and reduce the experimental cost of weapon systems. Compared with conventional weapons, guided weapon systems include seeker, navigation guidance and control system (hereinafter referred to as GNC system), engines, steering gear and other components, and the cost of flight experiments is very expensive. The use of hardware-in-the-loop simulation experiments can greatly reduce the number of flight experiments and reduce the cost of experiments. Compared with other simulations, hardware-in-the-loop simulation...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41G3/32
CPCF41G3/32
Inventor 李银海储海荣陈阳刘慧张玉莲
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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