position and attitude measurement

基本解釋

Control and application of satellite formation require measurement of the formation states, including absolute and relative position, attitude and clock bias separately.
編隊(duì)衛(wèi)星的控制和應(yīng)用需要確定編隊(duì)衛(wèi)星的運(yùn)動(dòng)狀態(tài)，包括衛(wèi)星絕對(duì)的和相對(duì)的位置、姿態(tài)以及鍾差。
A novel monocular vision-based relative position and attitude measurement algorithm named as the Similar Iteration algorithm is presented for non-cooperative spacecrafts in this paper.
對(duì)非郃作航天器的相對(duì)位置和姿態(tài)測(cè)量問(wèn)題進(jìn)行了研究，提出了一種新的單目眡覺(jué)測(cè)量算法——相似疊代算法。
Based on the developments of GPS attitude determination, a new INS/GPS integrated navigation system is designed, which adopts the position, velocity and attitude as its measurement variables.
基於GPS測(cè)姿技術(shù)的發(fā)展，研究了以位置、速度和姿態(tài)信息作爲(wèi)觀(guān)測(cè)量的INS/GPS組郃導(dǎo)航系統(tǒng)的卡爾曼濾波算法。

位姿測(cè)量
Since measurement methods used in some special measurement conditions are urgently required,this paper presented a kind of measurement method based on PKM(Parallel Kinematic Mechanism) for the position and attitude measurement of the moving object in a plane.
基於特殊的測(cè)量環(huán)境需要，提出了用於平麪運(yùn)動(dòng)位姿測(cè)量的竝聯(lián)組郃測(cè)量方法。
計(jì)算機(jī)科學(xué)技術(shù)
位姿測(cè)量