Full-link full-process simulation system and method for airborne infrared stabilized sighting system

A simulation system and full-link technology, which is applied in the field of full-link and full-process simulation system of airborne infrared stabilization system, can solve problems such as inability to complete signal flow transmission, inability to calculate the amount of misses, and incomplete links, etc., to achieve Dynamic simulation and signal flow transmission, convenient and accurate dynamic closed-loop simulation and target tracking, the effect of complete simulation link

Active Publication Date: 2014-12-03
XIDIAN UNIV
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AI Technical Summary

Problems solved by technology

The shortcomings of this system are: it does not consider the modeling of the target background, the modeling of the airborne stabilizing servo control system and the shaking of the carrier platform. When the system is applied to the airborne infrared imaging system, due to the lack of carrier platform simulation modules and machine The simulation module of load stabilization aiming servo control has

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  • Full-link full-process simulation system and method for airborne infrared stabilized sighting system
  • Full-link full-process simulation system and method for airborne infrared stabilized sighting system
  • Full-link full-process simulation system and method for airborne infrared stabilized sighting system

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Embodiment

[0056] Attached below figure 1 The system of the present invention is further described.

[0057] refer to figure 1 System block diagram of the system, the system of the present invention includes seven modules: target simulation module, background simulation module, environment simulation module, sensor simulation module, carrier platform simulation module, airborne stabilized aiming servo control simulation module and infrared image generation module; target simulation The module, the background simulation module, the environment simulation module, the sensor simulation module, the carrier platform simulation module, the airborne stabilization servo control simulation module and the infrared image generation module are connected through a bus;

[0058] The target simulation module includes a target geometric modeling unit and a target texture modeling unit; the target geometric modeling unit is used to establish the geometric model of the target, and the target texture mode...

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Abstract

The invention discloses a full-link full-process simulation system and method for an airborne infrared stabilized sighting system and aims to achieve full-link full-process simulation of the airborne infrared stabilized sighting system in laboratory conditions. The system comprises a target simulation module, a background simulation module, an environmental simulation module, a sensor simulation module, a carrier platform simulation module, an airborne stabilized sighting servo control simulation module and an infrared image generation module. The method includes the steps of 1, target simulation; 2, background simulation; 3, atmospheric effect simulation; 4, sensor effect simulation; 5, initial generation of infrared images; 6, judgment of whether a carrier platform is stabilized or not; 7, stabilized control simulation; 8, infrared target detection and tracking simulation; and 9, infrared image generation. The system has the advantages that considered links are complete, and dynamic simulation and signal stream transmission are achieved. The method has the advantage that infrared target tracking can be achieved.

Description

technical field [0001] The invention relates to the field of photoelectric imaging, in particular to a full-link and full-process simulation system and method of an airborne infrared stabilization system. Background technique [0002] The airborne infrared stabilization system is mounted on the aircraft, and the attitude change and vibration of the carrier aircraft will cause the instability of the boresight pointing, which will have a significant impact on the clear imaging of the observation equipment of the airborne infrared stabilization system. In order to overcome these effects, a visual axis stabilization subsystem must be established to isolate the visual axis of the optical sensor in the system from the movement and vibration of the carrier platform, so that the visual axis is stabilized in a fixed inertial space direction. At the same time, in order to be able to track and observe the observed target in real time, it is required that the airborne infrared stabiliza...

Claims

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Application Information

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IPC IPC(8): G06F17/50
Inventor 王晓蕊张宇琦徐立涛李奕吴颖霞王小兵袁宏学
Owner XIDIAN UNIV
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