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作 者:Kejiu, Mao Xu, Wang
机构地区:[1] Beijing Univ of Aeronautics and, Astronautics, Beijing, China
出 处:《Chinese Journal of Aeronautics》1990年第1期23-33,共11页中国航空学报(英文版)
摘 要:Static and dynamic mathematical models for a new type of engine and its actual hydraulic control system are proposed. A nonlinear mathematical model is used for the engine and afterburner fuel control system. With programs formed on the basis of these models, the static and dynamic close loop characteristics of this engine control system under afterburning condition have been analyzed in detail. Satisfactory results and valuable conclusions have been obtained. The results are useful for solving many practical problems of the engine control system.
关 键 词:Control Systems Hydraulic Drive DYNAMICS Mathematical Models
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