按稳定尾旋的条件对飞机运动方程组作了简化。
In this paper, the non-linear differential equations of aircraft motion are simplified by the condition of steady spin.
这些研究结果对于进一步研究大范围飞机运动控制系统的设计和实现提供了理论依据。
These results give a theoretical foundation for further studying the design and realization of control system of airplane's large_scale motion.
为了提高中程飞行冲突探测的精确性，有必要为飞机运动建立一个更精确的概率模型。
To increase the accuracy of mid-range conflict detection, designing a more ac-curate probabilistic model of aircraft motion is necessary.
为了提高气动参数辨识的精度，根据飞机运动方程，给出了测量中的系统偏差、尺度因子误差和随机噪声描述，并提出了一种飞行数据相容性检验的快速算法。
To get high accuracy of the identification of aerodynamic parameters, based on the motion equation of an aircraft, a fast algorithm for flight data compatibility check is presented in this paper.
为了提高气动参数辨识的精度，根据飞机运动方程，给出了测量中的系统偏差、尺度因子误差和随机噪声描述，并提出了一种飞行数据相容性检验的快速算法。
To get high accuracy of the identification of aerodynamic parameters, based on the motion equation of an aircraft, a fast algorithm for flight data compatibility check is presented in this paper.
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