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Autonomous orientation device and control method of autonomous orientation device

A technology of a directional device and a control method, applied in the directional field, can solve the problems of great influence of human factors, long operation time, and influence on the maneuverability of missiles, so as to achieve the effects of improving combat effectiveness, enhancing mobility, and shortening launch preparation time.

Inactive Publication Date: 2019-05-17
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] This manual operation method is greatly influenced by human factors and takes a long time to work. In particular, it is necessary to measure the geodetic coordinates of the erection positions of the laser autocollimator and the benchmarking instrument in advance, which affects the mobile launch capability of the missile.

Method used

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  • Autonomous orientation device and control method of autonomous orientation device
  • Autonomous orientation device and control method of autonomous orientation device

Examples

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Embodiment 1

[0079] figure 1 Shown is a schematic diagram of the overall structure of an autonomous orientation device 100 according to an embodiment of the present invention. The autonomous orientation device 100 includes: a laser self-collimation system 1 , a north-finding system 2 , an inclinometer 3 , three leveling feet 4 evenly distributed on the circumference, a leveling connection assembly 5 , and a translation system 6 . Wherein the inclinometer 3, the leveling leg 4 and the leveling connection assembly 5 together constitute a leveling system. The electronic communication and data processing circuits of each system in the device of the present invention are placed inside the box, and are not marked in this schematic diagram.

[0080] The laser autocollimation system 1 is installed above the north-seeking system 2, and the inclinometer 3 is installed below the north-seeking system 2. Through installation and calibration, the plumb axes of the three coincide and they are fixed toge...

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PUM

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Abstract

The invention discloses an autonomous orientation device. The autonomous orientation device comprises a north seeking system, a laser self-collimation system, an automatic leveling system and a translation system; the laser self-collimation system and the north seeking system are fixed, and the laser self-collimation system coincides with a plumb axis of the north seeking system; the north seekingsystem is disposed above the automatic leveling system, and the automatic leveling system can perform leveling on the north seeking system and the laser self-collimation system; the automatic leveling system is disposed on the translation system and can horizontally move along with the translation system; and the translation system performs translational motion when the laser self-collimation system sends a translation command to the translation system. The invention further discloses a control method of the autonomous orientation device. The autonomous orientation device and the control method can realize full-automatic autonomous orientation.

Description

technical field [0001] The invention relates to the field of orientation, in particular to an autonomous orientation device and a control method for the autonomous orientation device. Background technique [0002] During the launch of a rocket or missile, it is necessary to collimate and measure the prism on the projectile through the aiming device, measure the error angle in its azimuth, determine the initial azimuth information of the rocket or missile, establish the launch inertial coordinate system, and ensure the accuracy of the rocket or missile. launch accuracy. [0003] At present, laser autocollimators are usually used for azimuth measurement before rockets or missiles are launched. Before the measurement, the laser autocollimator and the benchmarking instrument are set up on two leveled support platforms respectively. The two support platforms are set up on two known geodetic coordinate points. The horizontal knob and azimuth knob of the instrument aim at the ben...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D3/12G01C15/00G01C17/00
Inventor 沈铖武王志乾刘畅李建荣刘绍锦于帅北蔡盛罗君
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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