Aerial turbofan engine switching control method, system and equipment
The invention relates to the technical field of turbofan engines, in particular to an aviation turbofan engine switching control method, system and equipment. The method comprises the steps that an aviation turbofan engine switching control system suitable for aircraft cruising is established; based...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention relates to the technical field of turbofan engines, in particular to an aviation turbofan engine switching control method, system and equipment. The method comprises the steps that an aviation turbofan engine switching control system suitable for aircraft cruising is established; based on the state of the aviation turbofan engine switching control system, a state-dependent switching mechanism is constructed; based on the state of the aviation turbofan engine switching control system, an undisturbed switching performance index is introduced, and an undisturbed switching mechanism is obtained; determining an event triggering sampling mechanism based on the state-dependent switching mechanism and the undisturbed switching mechanism; obtaining an undisturbed switching event triggering control scheme based on an undisturbed switching mechanism and an event triggering sampling mechanism; according to the state-dependent switching mechanism and the undisturbed switching event trigger control scheme, th |
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