Design method of aircraft nose wheel steering control box based on graphical model
A front wheel turning and design method technology, applied in general control systems, control/regulation systems, simulators, etc., can solve the problems that cannot meet the development needs of airborne electronic technology, the workload, difficulty and complexity are increased, and the airborne electronic The system structure is complex and other problems, so as to shorten the research and development cycle, improve the design quality, and ensure the accuracy.
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[0032] Attached below Figure 1-5 An embodiment of the present invention is described.
[0033] The invention describes the application of a graphical model-based design method in a certain aircraft nose wheel steering control box system. The aircraft nose wheel turning control box system receives the sensor and switch signal, performs logical operation according to the turning control law, outputs the control signal to drive the hydraulic system to control the turning of the aircraft nose wheel, and performs power-on self-test and periodic self-test at the same time. When the system fails Carry out fault response and send fault information to ground maintenance equipment.
[0034] The design method based on the graphical model realizes the decomposition and allocation of requirements and functions to the physical structure by constructing the requirements model and function model, and realizes the confirmation and verification of system requirements and function logic throug...
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