Applications to aerospace engineering are discussed , including introductory topics in orbital mechanics , flight dynamics , inertial navigation and attitude dynamics 亦将讨论动力学在航太工程上的应用，包含轨道力学，飞行力学，惯性导航与姿态动力学。
Strap - - down inertial navigation system ( sins ) is a kind of very advanced inertial navigation techno1ogy , and it is the deve1oping direct ion of inertia1 navigat ion 捷联式惯性导航系统是一种十分先进的惯性导航技术，是近年来惯性技术的一个发展方向。
Inertial navigation accelerometer is one of the important inertial instruments in the inertial system and its precision will directly influence the precision of inertial system 惯性导航加速度计是惯性系统中的重要元件之一,其精度直接影响惯性系统的精度。
This paper combines the wanderazimuth strapdown inertial navigation system with virtual instrument and designs a inertial navigation virtual instrument software 本论文以游移方位坐标系捷联式惯性导航系统为对象，与虚拟仪器技术结合起来，设计了一个惯性导航虚拟仪器软件。
Based on trajectory generation , sins digital algorithms and the vehicle - borne integrated navigation system are designed using object oriented design ( ood ) and c + + language ; hence simulated 在模拟航迹基础上，对捷联惯性导航算法和车载组合导航系统进行了面向对象的c + +程序设计和仿真。
Ths thesis first determines the research emphasis and principle boework by analyzing the development and present status of real - time operation system and inertial navigation system 本课题首先通过对实时操作系统及国内外惯性导航系统发展历史和现状的分析和透视，确定了软件设计的重点和总体框架。
On the other hand , inertial navigation must be integrated with extraneous information feedback to form a stable and closed - form integrated navigation system , so as to limit the error accumulation 另一方面,惯性导航必须引入外部信息反馈,形成稳定的闭环的组合导航系统,以抑制惯性导航误差的发散。
