舰船电子工程2019，Vol.39Issue(11)：176-180,212,6.DOI:10.3969/j.issn.1672-9730.2019.11.042
飞机的垂直机动边界性能研究
Research on Vertical Maneuvering Boundary Performance of Aircraft
摘要
Abstract
Based on the problem of insufficient research on vertical maneuvering boundary performance in the existing flight theory,this paper chooses the control law close to the actual flight,establishes the calculation model of vertical maneuvering,stud-ies the jack,half-jack roll and half-roll reversal motion,gives the calculation steps of vertical maneuvering boundary performance, and uses the platform of Matlab/Simulink. A numerical simulation program is compiled. Taking an aircraft as an example,the calcu-lation results are compared with the manual data,and the accuracy of the calculation model is verified. The boundary performance of vertical maneuvering is analyzed. The relationship between boundary velocity and height under different conditions and the boundary performance curve when ground height changes are given. The results can provide reference for the study of boundary performance of vertical maneuvering. The research method can also be extended to the study of vertical maneuvering boundary performance of other aircraft models,and has certain practical value.关键词
飞行性能/垂直机动/边界性能/SimulinkKey words
flight performance/vertical maneuver/boundary performance/Simulink分类
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潘军,陈柏松,华欣..飞机的垂直机动边界性能研究[J].舰船电子工程,2019,39(11):176-180,212,6.
