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Aircraft simulator for airborne weapon verification

A technology for airborne weapons and simulators, applied to simulators, simulators, instruments, etc. for space navigation conditions

Pending Publication Date: 2022-04-12
SHANGHAI INST OF ELECTROMECHANICAL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, there is no effective simulation verification platform for airborne weapon combat operation deduction and combat mode design. In the traditional equipment demonstration, a large number of simple scene settings and simplified model calculations are still used, and the deduction is carried out under specific combat process scenarios.

Method used

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  • Aircraft simulator for airborne weapon verification

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Embodiment Construction

[0024] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0025] A kind of airborne simulator oriented to airborne weapon verification provided by the present invention, refer to figure 1 , consisting of the following components:

[0026] Flight simulation subsystem: Simulate the aircraft take-off and landing and flight process. The flight simulation subsystem simulates the flight characteristics and flight status of the aircraft, establishes a 3- or 6-degree-of-freedom flight simulation model, calculates the maneuvering situation of the carrier aircraft in t...

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Abstract

The invention provides an aerial carrier simulator for airborne weapon verification. The aerial carrier simulator comprises a flight simulation subsystem for simulating the take-off, landing and flight process of an aircraft; the comprehensive avionics simulation subsystem is used for simulating the whole process of target detection, fire control calculation and airborne weapon launching of an avionics system; the visual simulation subsystem is used for simulating an aerial carrier cabin display instrument; and the aircraft simulation cabin is used for simulating aerial carrier cabin environment hardware. Aiming at the time sequence flow verification requirement before airborne weapon air launching, the aircraft piloting cabin and the flight process are simulated, the whole process of aircraft avionics system target detection, fire control resolving and weapon launching is vividly simulated, physical closing of a human-aircraft-airborne weapon system is achieved, and the aircraft avionics system can be simulated in real time. The real airborne weapon launching environment and process are simulated, and the airborne weapon system interface docking verification, launching separation verification and aircraft-missile cooperative verification capabilities are achieved.

Description

technical field [0001] The invention relates to the field of airborne weapon design and product verification, in particular to an airborne simulator for verification of airborne weapons. Background technique [0002] The combat use profile of airborne weapons is deeply coupled with the carrier platform, and the flight performance, mounting capability, detection capability, and perception capabilities of the carrier platform will all have an impact on the effectiveness of airborne weapons and equipment; the carrier aircraft as an airborne weapon The core element of combat use is not only the mounting, interaction and information support platform for realizing the combat capability of airborne weapons, but also an important part of the air battlefield environment. [0003] In a typical air combat encounter scenario, it is not only the flight performance, detection capabilities, and battlefield support capabilities of the loaded aircraft platform itself that affect the outcome ...

Claims

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Application Information

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IPC IPC(8): G09B9/00
Inventor 温超然李勇毕鹏尹航刘斯禹张顺家吴昕芸毛宇君
Owner SHANGHAI INST OF ELECTROMECHANICAL ENG
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