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CAN Bus Application Analysis in Launch Vehicle Control System
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Huan YU1, Xiaoming YAN1, Mingxin CHEN2, Feixiang ZHU1, Ming LI1
Missiles and Space Vehicles | 2024, 47(3) : 100 - 106
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Missiles and Space Vehicles | 2024, 47(3): 100-106
Test Control and Communication
CAN Bus Application Analysis in Launch Vehicle Control System
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Huan YU1, Xiaoming YAN1, Mingxin CHEN2, Feixiang ZHU1, Ming LI1
Affiliations
  • 1Shanghai Aerospace System Engineering,Shanghai,201108
  • 2Ningbo Space Engine Technology Co., Ltd,Wuhan,430040
Published: 2024-06-25 doi: 10.7654/j.issn.2097-1974.20240315
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With the development of data bus technology and the increasing demand for low-cost and high-reliability electrical systems in "flight-based transportation", Field Bus(FB) is gradually favored by the aerospace field. Controller Area Network(CAN), one of the most widely used field buses, has been researched and applied in missiles and tactical rockets. Considering the differences between launch vehicles and missiles, the application of CAN bus in launch vehicle control systems is expounded. The necessity of research is firstly analyzed, then typical CAN topologies suitable for medium and large-scale launch vehicles are given respectively. For the aim of practical use, two corresponding technologies are introduced which are the CAN relay technology and the CAN bus reconstruction. The efficiency and load rate of CAN bus are calculated which are then compared with the ones derived by 1553B data transmission under the same conditions. These results can be referenced by designers in a more accurate sense.

CAN bus  /  launch vehicle control system  /  CAN refactoring  /  CAN relay  /  1553B bus
Huan YU, Xiaoming YAN, Mingxin CHEN, Feixiang ZHU, Ming LI. CAN Bus Application Analysis in Launch Vehicle Control System[J]. Missiles and Space Vehicles, 2024 , 47 (3) : 100 -106 . DOI: 10.7654/j.issn.2097-1974.20240315
Year 2024 volume 47 Issue 3
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doi: 10.7654/j.issn.2097-1974.20240315
  • Receive Date:2022-05-30
  • Online Date:2025-07-04
  • Published:2024-06-25
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  • Received:2022-05-30
  • Revised:2023-07-01
Affiliations
    1Shanghai Aerospace System Engineering,Shanghai,201108
    2Ningbo Space Engine Technology Co., Ltd,Wuhan,430040
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
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占总种数比例
Percentage of
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种数
Number of
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占总种数比例
Percentage of total
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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