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Method and system for testing an alignment model of a submarine-launched missile inertial navigation platform

A platform and model technology, applied in the field of submarine-launched missile launch technology experiments, can solve the problems of large funds, huge system, high maintenance requirements, etc., and achieve the effect of low construction funds, simple maintenance and high use value

Active Publication Date: 2022-06-03
THE PLA NAVY SUBMARINE INST
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Problems solved by technology

The current test method is usually to build a reference azimuth transfer and platform alignment test system in the laboratory, and use a physical simulation test, that is, to build a reduced version of the missile's inertial navigation platform and alignment model in the laboratory. All terminals and servers require a lot of funds, the system is relatively large, and the maintenance requirements are also high

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  • Method and system for testing an alignment model of a submarine-launched missile inertial navigation platform
  • Method and system for testing an alignment model of a submarine-launched missile inertial navigation platform
  • Method and system for testing an alignment model of a submarine-launched missile inertial navigation platform

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Embodiment Construction

[0039] In order to make the objectives, technical solutions and advantages of the present invention clearer, the embodiments of the present invention will be further described in detail below with reference to the accompanying drawings.

[0040] The embodiment of the present invention provides a method for testing the alignment model of the submarine-launched missile inertial navigation platform, and the method can be implemented by a test system for the alignment model of the submarine-launched missile inertial navigation platform. like figure 1 As shown, the submarine-launched missile inertial navigation platform alignment model test system includes a terminal 1, a swing table controller 2, a swing table 3, a dynamic angle measurement device, an inclination angle control device 5, an inertial navigation platform simulator 6, and a dynamic angle measurement device. It includes a dynamic goniometer light pipe 4 and a photoelectric sensor assembly 7 , wherein a collimation mode...

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Abstract

The invention relates to a method and a system for testing an alignment model of a submarine-launched missile inertial navigation platform, and relates to the technical field of submarine-launched missile launching. The method is applied to the alignment model test system of the submarine-launched missile inertial navigation platform. The alignment model test system of the submarine-launched missile inertial navigation platform includes a terminal, a swing table controller, a swing table, a dynamic angle measuring device, and an inertial navigation platform simulator. In the embodiment of the present invention, the swing table controller controls the swing table to work, so that the swing table swings according to the set vertical and horizontal frequencies to generate pitch angle and roll angle information; start the stepping motor controller, and the stepping motor controls The controller controls the stepper motor to be in the tracking working state; the terminal conducts a semi-physical simulation test on the alignment model to be tested according to the alignment operation of the inertial navigation platform simulator and the swing table controller. The invention builds a semi-physical simulation experiment system under laboratory conditions, which can quickly verify the convergence of the collimation model to be tested.

Description

technical field [0001] The invention relates to the field of submarine-launched missile launching technology experiments, in particular to a method and a system for testing the alignment model of a submarine-launched missile inertial navigation platform. Background technique [0002] Submarine-launched missiles are called submarine-launched ballistic missiles, which refer to ballistic missiles launched by certain types of submarines. Before launching a submarine-launched missile, the inertial navigation platform of the missile needs to be initially aligned, that is, aiming at the position of the shooting target according to the collimation model, and then launch the missile. The alignment model needs to be tested before it can be used. The current test method is usually to build a reference azimuth transfer and platform alignment test system in the laboratory, and use physical simulation tests, that is, to build a reduced version of the missile inertial navigation platform ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C25/00F42B35/02
CPCG01C25/005F42B35/02
Inventor 杨海波王瑞臣李建林
Owner THE PLA NAVY SUBMARINE INST