The moment load is calculated by multiplying the total payload mass by the acceleration (due to gravity and due to the robot/gantry) by the distance of the payload's center of gravity to the rotating pinion.

彎矩負載的計算式：工作負載質量×加速度（由重力和機器人/門架系統(tǒng)引起）×負載重心到旋轉齒輪的距離。

Slide: Aluminum Bronze alloy, payload can be attached to top of slide or tooling plate.

幻燈片：鋁青銅合金黄色a片视频网导航，負載可以附加頂部或滑動工具板欧美国产日韩综合精品一区二区。

Experimental results show that this algorithm has obvious low complexity, high watermark payload and the strong robustness against compression, re- compression, antinoise and mean frames.

實驗結果證明該算法具有低計算復雜度和大容量水印承載能力，并具有很強的抗壓縮人人操人人色人人干人人舔、多次壓縮亚洲一区二区在线观看免费视频、抗噪聲的能力一级A片黄片免费视频。

In order to meet the requirements of light weights,high specific strength and high specific moduli for a space payload,the advantages and disadvantages of the engineering materials used in the supports of the space payload were analyzed,and the feasibility of the application of the carbon/epoxy composites to the support structures was explored.

為了滿足航天有效載荷輕型化美女黄毛A片免费观看、高比強度国产另类自拍、高比模量的要求，分析了航天有效載荷支撐結構常用工程材料的優(yōu)缺點国产爱福利一区；闡述了碳/環(huán)氧復合材料在航天有效載荷承力支撐結構中應用的可行性男人干男人的黄色视频；介紹了該材料在航天有效載荷中的實際工程應用及相關設計方法。

The goal of the network protocol is to deliver the sender's original payload to the recipient.

網(wǎng)絡協(xié)議的目標是把發(fā)送者的原始payload傳給接收者国产精品看片。

Andrea—Novel et al(1989),using the wave equation,derived a planar model for a gantry crane around the payload equilibrium position,which ignores the inertia of the payload and thinks of the cable as a perfectly flexible inextensible body.S.

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The acceleration profile of the crane motion is designed to induce minimum payload pendulation during transpo rt,while the deceleration stage is designed to ensure freed om of residual oscillation near the end of the transport,and to deliver the payload at the target point.The techniques induce payload pendulation at least one half ofan oscillation cycle or integer multiples during each of the acceleration and deceleration stages.Starr(1995)designed a symmetric two-step acceleration and deceleration profile to transfer a suspended object.The duration on the constant acceleration steps is assumed to be negligible relative to the period of the payload oscillation.A linear approximation method of the oscillation period is used to generate the two-step symmetric acceleration profile.

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General Dynamics will now work closely with the Department of National Defence in defining the scope of the LAV III upgrades. At the heart of the upgrade program is a high-capacity driveline and suspension that significantly increases the vehicle's payload. Increased payload will allow the vehicle the ability to deliver even better protection for Canadian soldiers.

通用動力現(xiàn)在與國防部在定義LAV III輕型裝甲車升級范圍上將進行緊密合作国产福利在线观看精品免费91啪，升級項目的核心是可以大幅提高有效載荷的高容量動力系統(tǒng)和懸掛系統(tǒng)天天插狠狠干，增加的載荷可以更好的為士兵提供保護。

The basic payload includes microwave datalink communications and camera with payload options comprising stabilised real-time day / night high resolution cameras, a full lighting rig that meets current maritime navigation standards, a loud-hailer system and a smoke marker launcher.

基本載荷包括微波數(shù)據(jù)鏈設備和照相設備视频一区视频二区国产激情，可選穩(wěn)定實時晝/夜高分辨率攝像頭精品福利岛国日韩AV，全向照明裝置，以滿足目前的海上航行標準欧美成年人片，還可以配置一個擴音器和煙霧標記發(fā)射器日本免费A网站。

In cooperation with the serial NSPO sounding rocket programs and application of the research results of the Institute of Aeronautics and Astronautics, National Cheng Kung University in the current proposal, we propose a series of Indigenous Propulsion Experiment payload Onboard Sounding Rockets, including: hydrazine monopropellant, hydrogen peroxide monopropellant, micro-propulsion and bipropellant subsystem. In the first stage of this multiple-year project, in two years (2005/4/1~2006/12/31) with two phases (phase I: 2005/1/1~2005/6/30 and phase II: 2005/7/1~2006/12/31) we will be compliant with the NSPO sounding rocket launch schedule of 2006 and develop the hydrazine thruster system onboard the sounding rocket as the payload to verify the key techniques and the thruster system developed.

本計畫第一階段預計以兩年時間(民國94年4月1日起至95年12月31日止)分兩期(第一期自民國94年4月1日起至94年9月30日止，第二期自民國94年10月1日起至民國95年12月31日止)配合NSPO的民國95年的探空火箭發(fā)射規(guī)劃時程日韩精品国语在线观看视频免费，發(fā)展聯(lián)胺單基推進器系統(tǒng)做為探空火箭酬載秋霞手机网，除了驗證自主發(fā)展的推進器系統(tǒng)與關鍵技術外，并進行高空實驗以進一步模擬測試該系統(tǒng)在高空環(huán)境與微重力狀態(tài)的性能特性r日本在线h。