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.
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。
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In this article, a quick method is presented to come up with the turning Angle and the turning point immediately, which can be applied to general turning-climb procedures.
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.