基本解釋[機(jī)械工程]姿態(tài)參數(shù)[航空、航天科學(xué)技術(shù)]姿態(tài)參數(shù)[天文學(xué)]姿態(tài)參數(shù)[測(cè)繪科學(xué)技術(shù)]姿態(tài)參數(shù)英漢例句雙語(yǔ)例句Finally, the iterative method was used to improve the precision of the attitude parameter of a target.最后，通過(guò)迭代提高目標(biāo)姿態(tài)解的精度。In order to determine the initial value of seat attitude parameter in 6 DOF function, an ejection seat all-attitude formula was presented in this paper.提出了彈射座椅全姿態(tài)關(guān)系式，介紹了在不同彈射條件下座椅全姿態(tài)關(guān)系式的取值范圍以及六自由度仿真中座椅姿態(tài)參數(shù)初始值的傳統(tǒng)選取方法。The paper parses the principle of measuring shield machine azimuth and deduces shield machine attitude parameter formulas based on TMB guidance system SLS-T from VMT Gmbh in Germany.以德國(guó)VMT公司的TMB制導(dǎo)系統(tǒng)SLS-T為例，主要解析了盾構(gòu)機(jī)軸線方位角測(cè)量原理，并完整地推導(dǎo)了盾構(gòu)機(jī)姿態(tài)參數(shù)公式。attitude parameter更多例句詞組短語(yǔ)短語(yǔ)attitude e parameter 姿態(tài)參數(shù)satellite attitude parameter 衛(wèi)星姿態(tài)orbit and attitude parameter 軌道及姿態(tài)參數(shù)risk attitude parameter 風(fēng)險(xiǎn)態(tài)度因子Position and Attitude Parameter Estimation 位姿參數(shù)估計(jì)attitude parameter更多詞組專(zhuān)業(yè)釋義機(jī)械工程姿態(tài)參數(shù)In view of the high speed spinning and the small caliber of High-speed Rotary Missile, the small diameter non-gyro posture parameter test system is designed, and the attitude parameter of missile aviation is tested and stored.本文針對(duì)高速旋轉(zhuǎn)彈高速自旋的特點(diǎn)和小口徑的測(cè)試要求,設(shè)計(jì)了無(wú)陀螺的小直徑姿態(tài)參數(shù)測(cè)試系統(tǒng),實(shí)現(xiàn)了彈體飛行全過(guò)程姿態(tài)參數(shù)的測(cè)試及存儲(chǔ)。航空、航天科學(xué)技術(shù)姿態(tài)參數(shù)天文學(xué)姿態(tài)參數(shù)測(cè)繪科學(xué)技術(shù)姿態(tài)參數(shù)