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Combined navigation controller

A combined navigation and controller technology, applied in the direction of weapon types, offensive equipment, projectiles, etc., can solve the problems of increasing the weight of guided shells, cumbersome quality, and affecting range

Pending Publication Date: 2021-09-14
重庆航天工业有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] The purpose of the present invention is to provide a combined navigation controller to solve the above problems in view of the traditional navigation controller which is bulky and heavy, which increases the weight of the whole guided projectile and affects the range.

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Embodiment Construction

[0020] The present invention will be further described below in conjunction with the accompanying drawings, but the present invention is not limited to the scope of the described embodiments.

[0021] The reference numerals in the drawings of the description include: control cabin housing 1, partition 12, upper chamber 11, lower chamber 13, boss 14, through hole 15, antenna 2, satellite receiver 3, IMU module 4, Main control board 5, bottom board 6.

[0022] see figure 1 with figure 2 , a combined navigation controller, comprising a control cabin housing 1, the overall control cabin housing 1 is a Von Karman curve structure, and is conformal to the missile body as a part of the missile body; the outer side of the control cabin housing 1 The antenna 2 is embedded, and the control cabin housing 1 is provided with a partition 12, and the control cabin housing 1 is divided into an upper chamber 11 and a lower chamber 13 by the partition board 12, and in the upper chamber 11 A ...

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Abstract

The invention discloses a combined navigation controller. The controller comprises a control cabin shell, and the whole control cabin shell is of a von Karman curve structure and serves as a part of a projectile body to be conformal with the projectile body. An antenna is embedded in the outer side of the control cabin shell, the control cabin shell is provided with a partition plate, the control cabin shell is divided into an upper cavity and a lower cavity through the partition plate, a satellite receiver is installed in the upper cavity, and an IMU module and a main control board are installed in the lower cavity. The combined navigation controller has the beneficial effects that the satellite receiver, the IMU module, the main control board and the antenna embedded in the outer side of the control cabin shell are integrated together, and the control cabin shell and the projectile body are conformal, so that modularization, miniaturization and combination of the combined navigation controller are realized, the size of the control cabin shell is effectively reduced, therefore, the size of the combined navigation controller is reduced, the weight of the guided projectile is further reduced, and the firing range is increased.

Description

technical field [0001] The invention relates to missile control technology, in particular to an integrated navigation controller. Background technique [0002] The integrated navigation controller is the core electronic device of the guided projectile control system, which plays a vital role in the flight process of the guided projectile. The navigation controller of the traditional intelligent ammunition combination has a complicated structure, resulting in bulky size and heavy weight, and increases the weight of the entire guided shell, which affects the firing range. Contents of the invention [0003] The purpose of the present invention is to provide a combined navigation controller to solve the problems of the traditional navigation controller which is bulky and heavy, which increases the weight of the whole guided shell and affects the range. [0004] In order to achieve the above object, the present invention adopts the following technical solutions. [0005] An i...

Claims

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Application Information

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IPC IPC(8): F42B10/60F42B10/38F42B10/42
CPCF42B10/60F42B10/38F42B10/42
Inventor 谭左红刘伟蔡奕袁鹏万小博郑瑞鑫张明星凌勇田圣尧李文彬樊勇
Owner 重庆航天工业有限公司
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