In this thesis, a great circular flight track generator is designed. Using the great circular flight track generator can generate the complex flight track.
本文提出了一种大圆飞行轨迹发生器的设计方案,按该方案设计的轨迹发生器可以通过设置航路点的位置(经度、纬度、高度)将飞机的机动飞行过程和巡航过程组合起来,以形成一条复杂飞行轨迹。
参考来源 - 机载组合导航技术研究·2,447,543篇论文数据，部分数据来源于NoteExpress
Finally, a simplified flight track model was proposed based on time step.
最后给出了根据时间步长推算的飞行轨迹简化计算模型。
The simulating results indicate that these flight path control laws can ensure the vehicle flies following the flight track of the towing plane.
计算结果表明，所采用的控制律可以实现运载器跟随拖曳飞机的飞行航迹。
The simulating results indicate that these static control laws can ensure the vehicle's equilibrium as it flies following the flight track of the towing plane.
仿真计算表明，所采用的控制律可以满足运载器飞行轨迹跟随拖曳飞机飞行轨迹时的飞行平衡特性。
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