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Inertial navigation system transfer vehicle

A technology of inertial navigation system and transfer vehicle, applied in general control system, control/adjustment system, trolley, etc., can solve problems such as instrument disturbance, affecting the accuracy of inertial navigation system, equipment falling, etc., and achieve a simple frame structure and convenient daily use , Lightweight and flexible design

Inactive Publication Date: 2018-09-14
中国人民解放军空军勤务学院
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] Regardless of the transfer method, due to the relatively long transfer distance, the equipment may fall during the transfer process, or the instrument may be disturbed by more torque in irregular directions, which will affect the accuracy of the inertial navigation system.

Method used

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  • Inertial navigation system transfer vehicle
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  • Inertial navigation system transfer vehicle

Examples

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Embodiment Construction

[0035] The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

[0036] Specific examples, such as figure 1 and figure 2 As shown, an inertial navigation system transfer vehicle includes a vehicle frame 1 and a load-bearing part, the load-bearing part is fixed on the top of the vehicle frame 1, and rollers are arranged at the bottom of the vehicle frame 1, and the described load-bearing part includes a horizontal tray 2 and an inertial The navigation system carrying box 3, the inertial navigation system carrying box 3 is arranged on the upper surface of the horizontal tray 2; it also includes a horizontal adjustment mechanism and a control mechanism. The horizontal adjustment mechanism includes screw stepping motors 4 located at the four corners of the vehicle frame 1, and the upper part of each screw stepping motor 4 is equipped with a Z-shaped screw hanging lug 5, one of the screw hanging lugs 5 The hor...

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Abstract

The invention relates to an inertial navigation system transfer vehicle. The transfer vehicle comprises a frame with a rectangular plane structure and a carrying part, the carrying part is fixed on the top of the frame, rollers are arranged at the bottom of the frame, the carrying part includes a horizontal tray and an inertial navigation system carrying box, and the inertial navigation system carrying box is arranged on the upper surface of the horizontal tray; a horizontal adjusting mechanism and a control mechanism are further included, the horizontal adjusting mechanism comprises screw stepping motors located at four corners of the frame, and the upper portion of each screw stepping motor is sleeved with a screw suspension loop; the control mechanism is arranged at the lower portion ofthe frame, the control mechanism includes a switch, a voltage regulator module, a battery, a single-chip computer, a gyroscope and a screw stepping motor driving module, and the battery supplies power to other electronic modules of the single-chip computer through a main power switch after the power passes through the voltage regulator module. The transfer vehicle has portable and flexible design, practicability, easy use and data acquisition and attitude adjustment functions.

Description

technical field [0001] The invention relates to the technical field of inertial navigation system transfer, in particular to an inertial navigation system transfer vehicle. Background technique [0002] A certain type of missile is one of the main air-to-ground precision guided weapons and equipment in active service in our army. As an important part of a certain type of missile, its inertial navigation system has an important impact on the performance and accuracy of the weapon and equipment. Post-inertial navigation system transshipment has been a thorny issue. A certain type of missile is my country's first-generation medium-range air-to-ground missile. Its combat mission is to avoid the enemy's ground air defense firepower and strike the enemy's high-value ground (water) surface fixed targets in depth. The missile adopts the guidance system of inertial mid-guidance and capture and control command TV terminal guidance. The inertial navigation system has high mid-guidance...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B62B3/02B62B3/04B62B5/00G05B19/042
CPCB62B3/02B62B3/04B62B5/0006B62B2202/41B62B2203/60G05B19/0423Y02P90/02
Inventor 陈伟李青张世豪张冰冰马超曾雪刚周弘扬
Owner 中国人民解放军空军勤务学院
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