Underwater unmanned platform aircraft autonomous test launch and control system

An aircraft, measurement, launch and control technology, applied in the aerospace field, can solve problems such as high maintenance cost and large-scale assembly, improve coverage and fault location accuracy, simplify electrical connection complexity, and enhance system rapid testing and parallel testing capabilities. Effect

Active Publication Date: 2017-01-04
THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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Problems solved by technology

Underwater platform weapon systems are an important military force of major maritime countries. However, manned platforms such as traditional submarines face h

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  • Underwater unmanned platform aircraft autonomous test launch and control system
  • Underwater unmanned platform aircraft autonomous test launch and control system

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[0017] In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.

[0018] figure 1 It is the overall structure diagram of the underwater unmanned platform aircraft autonomous measurement launch control system. The measurement, launch and control function of the autonomous measurement, launch and control system of the underwater unmanned platform aircraft is realized by the joint cooperation of the measurement, launch and control platform equipment 10 and th...

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Abstract

The invention discloses an underwater unmanned platform aircraft autonomous test launch and control system which comprises test launch and control platform equipment and aircraft equipment, wherein the test launch and control equipment is used for autonomously completing tests such as single item diagnosis and integrated testing on an aircraft by receiving corresponding instructions of platform remote-measuring equipment, and used for autonomously completing aircraft test launch and control and fault self-adaptive processing. Due to the solving ideas that autonomous tests of a system on the aircraft are adopted as main operation, and launch platform tests are adopted as auxiliary operation, and self testing and self diagnosis of the system of the aircraft can be achieved; meanwhile, a part of launch and control units are sufficiently minimized, and are transferred to the aircraft from the launch and control platform, so that aircraft emission control functions can be autonomously completed, the electric connection complicity of the aircraft and the launch and control system can be degraded, and the parallel launch and control properties of the system are improved.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to an autonomous measurement, launch and control system for an underwater unmanned platform aircraft. Background technique [0002] At present, most of the underwater launch vehicles need to be completed by human participation underwater. On the underwater platform, through manual operation of the measurement and launch control equipment, the launch and control process control of aircraft power supply and distribution, parameter binding, etc. is completed, and the application of underwater launch aircraft is realized. The underwater platform weapon system is an important military force of various maritime powers. However, manned platforms such as traditional submarines face high maintenance costs and difficulties in large-scale assembly. Their submarine-launched aircraft are generally used as underwater strategic nuclear deterrents. With the change of the marine envi...

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Application Information

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IPC IPC(8): G05B23/02
CPCG05B23/0213
Inventor 龙垚松席茂军王中苓王卓姚少君蒋金龙宋长哲丁波李冰张奎卢红海
Owner THE GENERAL DESIGNING INST OF HUBEI SPACE TECH ACAD
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