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.
经分析计算与试飞结果表明，对于爬升较缓慢的飞机，本控制方案可实现沿优化性能轨迹上升，并自动转入有利速度巡航。
It is shown that the climbing control plan is applicable to the aircraft with slower climbing according to optimum performance trajectory and automatically fly with optimum cruising velocity.
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