Control instruction generation device and method for profile test

Abstract

The invention discloses a control instruction generation device and method for a profile test, and belongs to the technical field of engineering tests. The device is characterized by consisting of a running control unit [1], a transverse instruction signal generation unit [2], a heading instruction signal generation unit [3], a longitudinal instruction signal generation unit [4], an auxiliary instruction signal generation unit [5], a system control bus [6], a signal definition and parameter setting application unit [7], a transverse instruction signal interface adaptor [8], a heading instruction signal interface adaptor [9], a longitudinal instruction signal interface adaptor [10] and an auxiliary instruction signal interface adaptor [11], wherein the running control unit [1] is used for executing a command of the signal definition and parameter setting application unit [7], and performing control operation on each instruction signal generation unit through the system control bus [6] to realize connection between each instruction signal generation unit and external equipment through the instruction signal interface adaptors corresponding to the instruction signal generation units. The device is complete in function, reasonable and compact in structure, convenient to use and high in extensibility and tailorability, and can work reliably.

Description

Technical field [0001] The invention relates to a control command generation device and method for profile tests, in particular to a control command generation device and method for profile tests realized by computer-controlled interface templates, and belongs to the technical field of engineering tests. Background technique [0002] Functional systems such as flight control system, hydraulic system, and landing gear control system play an increasingly important role in modern aircraft, especially with the application of fly-by-wire flight control technology and active control technology, the flight control system has reached the level of the aircraft. Overall, aerodynamics, structure, and strength are equally important and synchronized. At the same time, the safety and reliability of the flight control system are more important to the safety of the aircraft. In order to ensure the safety and reliability of the flight control system, the important way is to Carry out verific...

AI Technical Summary

Problems solved by technology

[0004] (1) For the operation of each single function, it is necessary to design a special actuator to simulate the driver's operation. For the operation of many different functions, it is necessary to design multiple special actuators to simulate the driver's operation, resulting in high Cost, long development and processing cycle;

[0005] (2) The special actuators are developed and produced for specific functional operations, and are not universal. After the specific functional operating status changes, adaptive changes, or even reprocessing and production are required;

[0006] (3) For complex operations with many different functions, it is difficult to design an executive mechanism for complex operations to simulate the driver's operation;

[0007] (4) The special actuator needs corresponding installation space, which is inconvenient to use;

[0008] (5) It is difficult to carry out unified coordination among multiple dedicated executive agencies

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