The invention discloses a rapid prototype
simulation method for an aero-engine
control system, belonging to the technical field of aero-engine
control system design. First establish the
control algorithm model, use
virtual instrument technology and real-time hardware platform to carry out the prototype design of the
control system, compile and download the designed aero-engine
control algorithm model to the real-time hardware platform through automatic
code generation technology, and quickly establish the
control algorithm prototype ;Secondly, the rapid control prototype is responsible for collecting the output
signal of the engine simulator after passing through the
signal interface unit, and calculates the relevant control quantities of the engine according to the control instructions and sends them to the engine simulator to realize the closed-
loop control of the engine; finally, the control
system The designer observes the
control effect in real time by monitoring the computer, continuously modifies the control
algorithm model according to the designer's performance requirements for the control
system, and repeats the closed-loop
simulation process of the rapid control prototype until the control
system designer's requirements are met.