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Ground test launch control system for test aircraft

An aircraft and remote control technology, applied in the sequence/logic controller program control, electrical program control and other directions, can solve the problems of poor internal coordination of the system, low system reusability, low reliability, etc., and achieve the development cost. The effect of reducing, enhancing system reusability, and improving performance indicators

Active Publication Date: 2016-02-17
HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aiming at the above defects and improvement needs of the prior art, the present invention provides a ground test launch and control system for test aircraft, which realizes the centralized control and data sharing of each system test on the arrow in a network manner, and realizes real-time processing and automatic interpretation of test data , to complete the full-process comprehensive test and launch task of the test aircraft, the purpose is to realize the integration of test and simulation equipment based on the ground test launch control system of the control system, thereby solving the problem of poor compatibility and reliability of the current ground test system Low, low system reusability, and poor internal coordination capabilities of the system and other technical problems

Method used

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  • Ground test launch control system for test aircraft

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Embodiment Construction

[0016] In order to make the object, technical solution and advantages of the present invention clearer, 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.

[0017] The ground test launching and control system of the experimental aircraft of the present invention adopts the distributed design of the front and back, and is composed of the field test equipment at the front, the client terminal at the back, and the communication equipment. The front-end console of the system is mainly used for direct electrical connection with the test aircraft to reali...

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Abstract

The invention discloses a ground test launch control system for a test aircraft, and belongs to the technical field of ground tests, launch and control over test aircrafts. In the prior art, in a control system for the test aircraft, a simulation system, a test system and a launch control system are respectively arranged, or even multiple ground test systems are arranged, and all the test systems are large in software and hardware difference and not uniform in technological path. The launch control system comprises a launch control panel and a remote control panel, network communication is adopted, the launch control panel comprises a test host module, CPCI bus specification design is adopted for the test host module, a test host of the test host module is formed by configuring a standard CPCI case, a digital quantity standard function board card, an analog quantity standard function board card and a synchronous serial port function board card, all needed test modules of the system are arranged according to the CPCI bus standard, and therefore the maturity of software is higher. The development cost of the system is greatly reduced, the compatibility and reliability of the system are improved, and the reusability of the system is enhanced.

Description

technical field [0001] The invention belongs to the technical field of test aircraft ground testing, launch and control, and more specifically relates to a test aircraft ground test launch control system. Background technique [0002] At present, there are generally one or more sets of ground test systems for the simulation, test and launch control of the test aircraft control system. The software and hardware of each test system are quite different, and the technical paths are different. This self-contained test mode of each system is gradually formed with the development of the technology of the product to be tested, which brings convenience to the development and management of the system. However, with the continuous improvement of testing and launch technology requirements for the products to be tested, the cost requirements are becoming more and more stringent. The technical level of the test system is uneven, and the standards are not uniform, resulting in poor compat...

Claims

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Application Information

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IPC IPC(8): G05B19/04
CPCG05B19/04
Inventor 张伟吴旭亮琚俊梅姜娜
Owner HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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