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Control system used for fixed wing canard rudder

A control system and fixed-wing technology, applied in the aerospace field, can solve the problems of complex control and high cost, and achieve the effects of improving the accuracy of landing, high cost-effectiveness ratio, and reducing volume and cost

Inactive Publication Date: 2017-06-20
BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the prior art, it mainly uses the cross duck rudder to realize the precise guidance of the projectile, but this method is costly and the control is relatively complicated

Method used

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  • Control system used for fixed wing canard rudder
  • Control system used for fixed wing canard rudder
  • Control system used for fixed wing canard rudder

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Embodiment Construction

[0026] In order to make the objectives, technical solutions, and advantages of the present invention clearer and more comprehensible, the present invention will be further described in detail below with reference to the accompanying drawings and preferred embodiments. However, it should be noted that many details listed in the specification are only to enable the reader to have a thorough understanding of one or more aspects of the present invention, and these aspects of the present invention can be implemented even without these specific details.

[0027] This embodiment provides a control system for a fixed-wing canard, and its schematic diagram is as follows figure 1 As shown, it includes a control mechanism system, an attitude measurement system, a wireless communication system and a processor; the control system replaces the head fuze of the mortar shell and is installed on the head of the mortar shell.

[0028] The attitude measurement system of this embodiment can be realized...

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Abstract

The invention discloses a control system used for a fixed wing canard rudder, and the control system replaces the head of a mortar projectile to fuze, and is mounted on the head of the mortar projectile. The control system comprises a control mechanism system, an attitude measurement system, a wireless communication system and a processor, wherein the control mechanism system comprises electronic load, a rectifying bridge and a permanent magnet motor; the attitude measurement system is used for transmitting acquired rolling angular velocity to the processor through the wireless communication system; the processor is used for controlling the electronic load according to rotation speed difference between the wing canard rudder and a projectile body; and electromagnetic torque of the permanent magnet motor is regulated through the rectifying bridge, so that rolling angular velocity of the fixed wing canard rudder is changed. According to the control system disclosed by the invention, the electromagnetic torque of the permanent magnet motor and the rolling angular velocity of the fixed wing canard rudder are changed, so that the control force vector direction of the canard rudder is changed; mass centre motion is corrected by motion around a mass center, so that fall point precision of the mortar projectile is improved; and moreover, a conventional servo mechanism is cancelled, so that the size and the cost of the control system can be greatly reduced, and therefore, the control system has the characteristic of a high cost-benefit ratio.

Description

Technical field [0001] The invention relates to the field of aerospace, in particular to a control system for a fixed-wing canard. Background technique [0002] Mortar has the characteristics of curved trajectory, fast rate of fire, simple structure, convenient maneuverability, and easy operation. It is suitable for urban street fighting and mountain warfare, and has been widely used in countries all over the world. In the prior art, the cross duck rudder is mainly used to realize the precise guidance of the projectile, but this method has high cost and relatively complicated control. Summary of the invention [0003] In view of the above-mentioned defects in the prior art, the present invention provides a control system for a fixed-wing canard, which improves the accuracy of the landing point of the mortar. [0004] The present invention provides a control system for a fixed-wing canard. The improvement is that the control system includes a control mechanism system, an attitude me...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B10/64
CPCF42B10/64
Inventor 张衍儒肖练刚邱奕周华孙凯白璐
Owner BEIJING AEROSPACE AUTOMATIC CONTROL RES INST
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