inertial coordinate system

基本解釋

A dynamic model of landing gear struts is introduced in a non-inertial coordinate system.
在非慣性坐標系中建立了起落架支柱的動力學模型。
A gyrobondgraph method for the dynamic and static force analysis of planar linkage in non-inertial coordinate system is introduced.
介紹非慣性系平麪連桿機搆動態(tài)靜力分析的廻轉鍵郃圖法。
In this paper, the mathematics model of SINS in the Launch Inertial Coordinate System is established, and the error propagation function.
論文建立了發(fā)射慣性坐標系中的SINS導航解算模型，推導了該坐標系中的SINS誤差傳播方程。

慣性坐標系
According to orbit control theory, attitude control theory and kinetic theory, the output of 3-axis ultraviolet attitude reference sensor was determined. The result is angle of aircraft in the geocentric inertial coordinate system.
根據空間飛行器控制中的軌道控制原理、姿態(tài)控制原理和動力學原理,確定了紫外三軸姿態(tài)敏感器的測量輸出量,這就是飛行器在地心慣性坐標系中的角度。
物理學
慣性坐標系