Aircraft reconnaissance and attack control launching system

A launch system and aircraft technology, applied in the field of aircraft, can solve problems such as inflexible launch load control and easy loss of targets, and achieve the effects of eliminating potential safety hazards, reducing flight attitude requirements, and fast loading and unloading

Pending Publication Date: 2018-11-16
TIANJIN AEROSPACE ZHONGWEI DATA SYST TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] In view of this, the present invention aims to propose an aircraft reconnaissance and attack control launch system to solve the problem that the existing aircraft is inflexible in the control of the launch load during the reconnaissance and attack process, and it is necessary to manually track the target and easily lose the target.

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  • Aircraft reconnaissance and attack control launching system
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  • Aircraft reconnaissance and attack control launching system

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Embodiment Construction

[0056] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0057] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "upper", "lower", "front", "rear", "left", "right", " The orientations or positional relationships indicated by "vertical", "horizontal", "top", "bottom", "inner" and "outer" are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and Simplified descriptions, rather than indicating or implying that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and thus should not be construed as limiting the invention. In addition, the terms "first", "second", etc. are used for descriptive purposes only, and should not be understood ...

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Abstract

The invention provides an aircraft reconnaissance and attack control launching system which comprises an aircraft body. A mounting device is installed on the body and used for installing launching loads. The launching loads are correspondingly provided with fire control units and servo control units connected with the fire control units. The servo control units are used for adjusting the pitchingand direction angles of the launching loads. The fire control units are connected with flight control units through communication interfaces. The flight control units are connected with a ground station through wireless communication modules. The aircraft reconnaissance and attack control launching system is provided with launching load attitude adjustment devices which are the servo control units, the pitching and direction attitudes of the launching loads can be adjusted, a target can be attacked within a certain range without adjustment of the multi-rotor attitude, task execution flexibility is high, and all-directional multi-angle attacks can be achieved.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to an aircraft detection and attack control launching system. Background technique [0002] With the rapid development of UAV technology at home and abroad, the types and uses of UAVs are becoming more and more diverse, especially the rapid development of multi-rotors, which have vertical take-off and landing, fixed-point hovering, simple mechanical structure, high safety, With the advantages of low cost, it can be equipped with multi-purpose equipment such as visible light and infrared thermal imaging cameras, and is widely used in power line inspection, surveying and mapping, fire protection, anti-terrorism, aerospace and other fields. [0003] In the field of anti-terrorism, multi-rotors can be used in reconnaissance and strike missions. The applications are mainly focused on reconnaissance missions, and rarely used in strike missions, and the strike range is limited...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D1/06
CPCB64D1/06
Inventor 徐雷雷徐凯樊昊薛赛男贾意弦张国荣张楠王慧王霖李兆晨
Owner TIANJIN AEROSPACE ZHONGWEI DATA SYST TECH CO LTD
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