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Near space reconnaissance, supervision, management and control system

A near space, control system technology, applied in the field of unmanned fixed-wing aircraft, can solve the problems of small satellite communication bandwidth, short line-of-sight communication distance, high energy consumption, etc., and achieve the effect of reducing the demand for flight sites and saving energy

Inactive Publication Date: 2018-07-31
CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to ground take-off, the energy consumption is relatively large, and the current fixed-wing aircraft with ground take-off has a short line-of-sight communication distance and a small satellite communication bandwidth.

Method used

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  • Near space reconnaissance, supervision, management and control system
  • Near space reconnaissance, supervision, management and control system
  • Near space reconnaissance, supervision, management and control system

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Embodiment Construction

[0023] The embodiments of the present invention are described in detail below. This embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and specific operating procedures are provided, but the protection scope of the present invention is not limited to the following implementation example.

[0024] figure 1 Shown is a schematic structural diagram of the near space detection, monitoring and control system described in the embodiment of the present invention. The near-space detection, monitoring and control system described in this embodiment includes an aerostat 101 and a fixed-wing aircraft storage box 102 , and the aerostat 101 and the fixed-wing aircraft storage box 102 are connected by a cable 103 . The outer surface of the storage box 102 is wrapped with a solar panel 104 to provide energy for the system.

[0025] figure 2 Shown is a schematic diagram of communication between the system and the...

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Abstract

The invention discloses a near space reconnaissance, supervision, management and control system, and the system comprises an aerostat (101) and a fixed-wing aircraft storage box (102). The fixed-wingaircraft storage box (102) is fixedly connected below the aerostat (101), and the interior of the fixed-wing aircraft storage box (102) is provided with a fixed-wing aircraft (301). After the fixed-wing aircraft storage box (102) receives an instruction to open a box door (302), the fixed-wing aircraft (301) converts potential energy into kinetic energy for autonomous flight. Meanwhile, after theweight withstood by the aerostat (101) is reduced, the aerostat (101) starts to rise and then arrives at a near space. Compared with the prior art, the system has the following advantages that the system enables the fixed-wing aircraft (301) or other loads to be carried to a specified flight height through the effective use of the floating force of the aerostat (101), reduces the demands for a flight place, can rise to a certain height under the condition that the fixed-wing aircraft (301) does not need to start, and saves the energy.

Description

technical field [0001] The invention relates to an unmanned fixed-wing aircraft, and more particularly to a reconnaissance, monitoring and control system for near space. Background technique [0002] At present, with the gradual maturity of unmanned fixed-wing aircraft technology, the fixed-wing aircraft can carry different loads to complete different tasks as a platform. Generally, the fixed-wing aircraft is launched from the ground airport by the ground system command, and the ground station passes the line-of-sight Communication or satellite communication remote command to execute remote tasks. Due to the high energy consumption of ground takeoff, and the current fixed-wing aircraft taking off from the ground has a short line-of-sight communication distance and a small satellite communication bandwidth. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide an energy-saving near-space reconnaissance, monitoring and ...

Claims

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Application Information

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IPC IPC(8): G05D1/10B64B1/00B64C39/02
CPCG05D1/101B64B1/00B64C39/02B64U10/30B64U70/20B64U10/25
Inventor 荣海春徐亮
Owner CHINA ELECTRONIC TECH GRP CORP NO 38 RES INST