用航迹角来代替性能计算中常用的爬升率概念，对飞机爬升各项参数的变化及其影响因素进行了研究。
In this article, trajectory angle is taking the place of the rate of climb in order to study the influence of other trajectory parameter applied on it.
以涡轮和火箭冲压组合动力的工作模式以及飞行器飞行航迹角、迎角等为调参量，构造空天飞行器爬升轨迹优化流程。
The flow chart of optimizing ASP climb track is designed by adjusting some parameters of Euler angle, attack angle, turbine and rocket-ramjet combined cycle work models, etc.
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