Apparatus and method for testing aircraft message trigger logics
First Claim
1. A test apparatus, independent of an aircraft, for testing aircraft message trigger logic for the aircraft, comprising:
- a DFDAU (Digital Flight Data Acquisition Unit), which is configured to receive message trigger logic to be tested, wherein the message trigger logic is loaded onto the DFDAU;
an input interface, which is configured to receive data of aircraft condition; and
a simulation signal generator, which is connected to the input interface and configured to generate a simulation signal according to the data of aircraft condition, wherein a type and property of the simulation signal is identical to those of aircraft signals collected by aircraft sensors and data transmitted from other assemblies of aircraft condition;
wherein, the DFDAU is further configured to receive the simulation signal and generate a message according to the message trigger logic to be tested based on the simulation signal;
wherein the simulation signal generator comprises at least one of a discrete signal generation unit, a voltage signal generation unit, an analog signal generation unit or a bus signal generation unit;
wherein the input interface is connected to at least one of the discrete signal generation unit, the voltage signal generation unit, the analog signal generation unit or the bus signal generation unit via a bus system; and
a wiring extension device comprising a wiring board.
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Abstract
According to various embodiments, the present invention relates to a platform and method for testing aircraft message trigger logics are disclosed. Apparatus for testing message trigger logics of aircraft comprises: DFDAU (a Digital Flight Data Acquisition Unit), which is adapted to receive message trigger logics to be tested; an input interface, which is adapted to receive data of aircraft condition; and a simulation signal generator, which is adapted to generate simulation signals according to the data of aircraft condition; wherein, the DFDAU is adapted to receive the simulation signals, and generate messages according to the message trigger logics to be tested.
11 Citations
22 Claims
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1. A test apparatus, independent of an aircraft, for testing aircraft message trigger logic for the aircraft, comprising:
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a DFDAU (Digital Flight Data Acquisition Unit), which is configured to receive message trigger logic to be tested, wherein the message trigger logic is loaded onto the DFDAU; an input interface, which is configured to receive data of aircraft condition; and a simulation signal generator, which is connected to the input interface and configured to generate a simulation signal according to the data of aircraft condition, wherein a type and property of the simulation signal is identical to those of aircraft signals collected by aircraft sensors and data transmitted from other assemblies of aircraft condition; wherein, the DFDAU is further configured to receive the simulation signal and generate a message according to the message trigger logic to be tested based on the simulation signal; wherein the simulation signal generator comprises at least one of a discrete signal generation unit, a voltage signal generation unit, an analog signal generation unit or a bus signal generation unit; wherein the input interface is connected to at least one of the discrete signal generation unit, the voltage signal generation unit, the analog signal generation unit or the bus signal generation unit via a bus system; and a wiring extension device comprising a wiring board. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18)
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19. A method for testing aircraft message trigger logic, the method implemented by a test apparatus comprising:
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a DFDAU (Digital Flight Data Acquisition Unit), which is configured to receive message trigger logic to be tested, an input interface, which is configured to receive data of aircraft condition, and a simulation signal generator, which is connected to the input interface and configured to generate a simulation signal according to the data of aircraft condition, wherein a type and property of the simulation signal is identical to those of aircraft signals collected by aircraft sensors and data transmitted from other assemblies of aircraft condition; the method comprising; loading the message trigger logic onto the DFDAU; loading the data of aircraft condition composed according to aviation communication standard or data of aircraft condition from QAR, via the input interface, wherein the data of aircraft condition may trigger the message trigger logic to be tested; generating, by the simulation signal generator, the simulation signal according to the data of aircraft condition, and connecting the simulation signal into the DFDAU; generating, by the DFDAU, a message in response to the simulation signal connected to the DFDAU when data in the simulation signal triggers the message trigger logic; and determining whether the message trigger logic is correct according to the message generated by DFDAU. - View Dependent Claims (20, 21, 22)
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Specification