查询词典 inertial

A method to drive dipe by using inertial navigation is discussed in this paper. The mathermetic model ofinclination survey system, wnich codsis of three accelerometers and three magnetometers, and an approachto realize it are presented.

本文根据飞机定向的方法，讨论了惯性导航系统在确定油井姿态中的应用，并且推导出了由三个加速度计和三个磁通门构成的测斜系统的数学模型以及测斜系统的实现方法。

Near the mesopause, propagating in the background wind which increasing with heights, the inertial gravity waves will reach their critical layers.

在中层顶附近，在随高度增加的背景风中传播的惯性重力波会遇到临界层。

A guidance and control method of applying BTT technology to the inertial guidance part for winged missile are presented.

提出了将通常用于寻的导弹控制的BTT技术用于飞航导弹惯性制导段的有关制导与控制理论和方法。

In order to develop better and lighter inertial guidance and control system, people began to develop more complicated electronic components, which has facilitated the development of solid-state electronics.

为了获得更好、更轻的惯性制导和控制系统，人们开始研制复杂的电子器件，结果带动了固态电子学的发展。

A missile 's inertial guidance system.

导弹惯性制导系统。

Survey is made of study and testing methods of microyield strength of beryllium materials used in inertial guidance instrument.

介绍了惯性器件用铍材微屈服强度的研究概况、测试方法，讨论了晶粒尺寸、杂质、热处理与微合金化等对铍材MYS的影响。

Since the information of multi peaks and inertial guidance are introduced, the robust of algorithm and probability of matching are improved effectively.

有关下视景象匹配中图像的预处理和配准相似性度量和搜索算法已有较多的文献发表，其综

A further development of the DF-5 is the DF-5A, with a range augmentation to over 13,000 km and an improved inertial guidance system.

DF-5进一步发展是DF-5A，具有超过13，000公里的增大射程和一个改进惯性制导系统。

This system has the advantages of high operation speed and high discrimination. The cost will be low due to the betterment of missile inertial guidance system.

该系统具有光学系统运算速度快，对畸变目标识别能力高等优点，在导弹原有惯性制导系统上进行改进，成本低。

Based on the study of the system model in different flight conditions, and by use of real-time compensation in inertial guidance, a method is put forward for selecting the error compensation model and the model of compensation evaluation based on the engineering background.

通过研究飞行工作环境变化导致的系统模型差异，结合惯性制导实时补偿方法，提出了基于工程背景的误差补偿和补偿评估模型的选取方法。

The split between the two groups can hardly be papered over.

这两个团体间的分歧难以掩饰。

This approach not only encourages a greater number of responses, but minimizes the likelihood of stale groupthink.

这种做法不仅鼓励了更多的反应，而且减少跟风的可能性。