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A space intelligent attitude control aircraft

A technology of space intelligence and aircraft, applied in the direction of aerospace vehicle guides, weapon types, structural parts, etc., can solve the problems of unfavorable popularization and application, large size, large quality, etc., achieve clear electrical interface, improve product reliability, and facilitate Effects of Assembly and Troubleshooting

Active Publication Date: 2019-12-20
BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Usually, for the detection of space targets, observation of target characteristics, search, tracking and targeting, or precise strikes, relatively large integrated space platforms for attitude and orbit control are used, such as satellite platforms and relatively large space vehicles. , high quality and high cost, which is not conducive to popularization and application

Method used

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  • A space intelligent attitude control aircraft
  • A space intelligent attitude control aircraft
  • A space intelligent attitude control aircraft

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Embodiment Construction

[0022] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0023] The invention is a small space intelligent attitude control aircraft, which adopts modularization and platform design ideas, and realizes miniaturization, generalization and high reliability of the device.

[0024] 1. Structural composition and working principle description

[0025] The small space intelligent attitude control aircraft is designed as a slender cylindrical structure, such as figure 1 shown. The slenderness ratio is about 2:7. The cylindrical shape structure is convenient for installation and launch in the launch tube. The overall layout of the aircraft is designed as a modular structure, and the entire aircraft includes a power supply compartment 1, an engine compartment 2, a control combination compartment 3 and a load compartment 4. Each module is connected axially in series from the head of the aircraft to the ta...

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Abstract

The invention provides a space intelligent attitude control aircraft, which includes a power supply compartment for powering other compartment equipment, a load compartment for loading load equipment, an engine compartment, and according to the mission requirements and the attitude of the aircraft, the engine compartment through the engine compartment The switch is the control combination cabin that realizes the attitude control of the roll, yaw, and pitch of the aircraft. The load cabin, the control combination cabin, the engine compartment, and the power supply compartment are connected in series from the aircraft head to the aircraft tail along the aircraft axis, wherein the engine compartment There is no cabin shell, and its engine is directly exposed. The invention adopts the idea of ​​modularization and platform design, and realizes the miniaturization, generalization and high reliability of the device.

Description

technical field [0001] The invention relates to a space intelligent attitude control aircraft, which is used for space target characteristic measurement, space target detection, observation, search, tracking and aiming or precision strike and the like. It belongs to the technical field of space detection and defense penetration. Background technique [0002] Usually, for the detection of space targets, observation of target characteristics, search, tracking and targeting, or precise strikes, relatively large integrated space platforms for attitude and orbit control are used, such as satellite platforms and relatively large space vehicles. , high quality and high cost are unfavorable for popularization and application. Contents of the invention [0003] The technical problem of the present invention is: to overcome the deficiencies of the prior art, design a space intelligent attitude control aircraft, realize the precise control of the attitude of the aircraft itself, and...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F42B15/01B64G1/24H01M2/10H01R13/46H01M50/20
CPCH01R13/46F42B15/01B64G1/24H01M50/20Y02E60/10
Inventor 杨金鹏邵春收刘成国王春莉焦胜海李建新黎良刘生东刘天博张雪峰陈晓光段雅丽单喜军秦丽华邹晓风张娟刘郁笑
Owner BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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