Development of Test Equipment for Airborne Missile Launch Control System Based on Virtual Instrument Technology

DOI

10.2991/macmc-17.2018.88How to use a DOI?

Keywords

Airborne missile, Launch control system, Test equipment; Virtual instrument; Fault test

Abstract

The missile launching control system is the core equipment of an air to ground missile fire control system, and the equipment equipped with the original test equipment has the problems of single function and low level of integrated support, so a new type of test equipment for airborne missile launch control system is developed by combining virtual instrument technology and traditional test methods. The main control computer is taken as the core of the system, the VC++ language is used to program, and many technologies are adopted such as the standard interface and bus technology, the virtual instrument technology, the fault test technology and the FIFO technology and so on. The test equipment has many advantages of reliable and stable operation, high accuracy and good expansibility. The automation level of test equipment is improved effectively. So the test equipment has certain practicability and promotion value.

Copyright

© 2018, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Xiaoyu Zhang
AU  - Guifang Cai
PY  - 2018/01
DA  - 2018/01
TI  - Development of Test Equipment for Airborne Missile Launch Control System Based on Virtual Instrument Technology
BT  - Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017)
PB  - Atlantis Press
SP  - 473
EP  - 479
SN  - 2352-5401
UR  - https://doi.org/10.2991/macmc-17.2018.88
DO  - 10.2991/macmc-17.2018.88
ID  - Zhang2018/01
ER  -