Control box for aircraft data forwarding and launching control
The invention provides a control box for aircraft data forwarding and launching control. A core board receives a control instruction of an upper interface connector, parses and recombines the controlinstruction, and judges the parsed control instruction corresponding to the upper interface connector...
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Format | Patent |
Language | Chinese English |
Published |
28.04.2020
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Subjects | |
Online Access | Get full text |
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Abstract | The invention provides a control box for aircraft data forwarding and launching control. A core board receives a control instruction of an upper interface connector, parses and recombines the controlinstruction, and judges the parsed control instruction corresponding to the upper interface connector: if the parsed control instruction is a power supply instruction, the core board provides power for an external aircraft through a lower interface connector; if the instruction is the control instruction, the core board forwards the control instruction through the lower interface connector; and the core board receives the state information of the external aircraft through the lower interface connector, analyzes and recombines the data, updates the state information of the aircraft, and judgeswhether a fault occurs according to the state of the aircraft: if the external aircraft has the fault, the core board immediately disconnects the power supply of the aircraft. The control box has thefunctions of multi-path con |
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AbstractList | The invention provides a control box for aircraft data forwarding and launching control. A core board receives a control instruction of an upper interface connector, parses and recombines the controlinstruction, and judges the parsed control instruction corresponding to the upper interface connector: if the parsed control instruction is a power supply instruction, the core board provides power for an external aircraft through a lower interface connector; if the instruction is the control instruction, the core board forwards the control instruction through the lower interface connector; and the core board receives the state information of the external aircraft through the lower interface connector, analyzes and recombines the data, updates the state information of the aircraft, and judgeswhether a fault occurs according to the state of the aircraft: if the external aircraft has the fault, the core board immediately disconnects the power supply of the aircraft. The control box has thefunctions of multi-path con |
Author | YANG LONGJUN YAO KANGSHENG ZHANG YI MA WEI ZHANG HONGYU TONG QIN YU YOUHAO XIONG PAN XIONG JING SHI LIN LIU HONGLING FU HONGFEI LUO YUN WANG FAN |
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DocumentTitleAlternate | 飞行器数据转发和发射控制的控制盒 |
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Notes | Application Number: CN201911238156 |
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Snippet | The invention provides a control box for aircraft data forwarding and launching control. A core board receives a control instruction of an upper interface... |
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SubjectTerms | CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING |
Title | Control box for aircraft data forwarding and launching control |
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