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Contents:2024,Vol:29,Issue(2):115-128 |
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Citation: |
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ZHANG Haowen, GUAN Hongyang, WANG Shuangjia. Design of MC9 Test Equipment for Inertial Reference System[J]. International Journal of Plant Engineering and Management, 2024, 29(2): 115-128 |
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| Design of MC9 Test Equipment for Inertial Reference System |
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| ZHANG Haowen, GUAN Hongyang, WANG Shuangjia |
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| AVIC Xi'an Flight Automatic Control Research Institute, Xi'an 710076, China |
| Abstract: |
| Inertial reference system is one of the airborne equipment. According to the requirements of SAE ARP4754A Guidelines for Development of Civil Aircraft and Systems, MC9 equipment qualification test is needed to verify that the inertial reference system can perform reservation function under specified service conditions. That is, the inertial reference system shall pass certain environmental tests specified in DO-160G. Some tests are faced with the problem that the test equipment should have the function requirements of isolation protection and load simulation. Therefore, a kind of test equipment which can provide isolation protection and simulate load function in the test is designed. |
| Key words:
inertial reference system
MC9
isolation protection
simulated load
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| Received: 2024-05-01
Revised:
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| DOI: 10.13434/j.cnki.1007-4546.2024.0204 |
| Corresponding author:
Email： |
| Author description:
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References: |
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[1] SAE. Guidelines for development of civil aicraft and systems[S]. United States:SAE International, 2010.
[2] Civil Aviation Administration of China. Model qualification approval procedure[S]. Beijing:Airworthiness Approval Division, Civil Aviation Administration of China, 2023.(in Chinese)
[3] Radio Technical Commission for Aeronautics. Environmental con-ditions and test procedures for airborne equipment[S]. Washington, D.C.:RTCA, 2010. |
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