轨道机动的英文

• orbital maneuver
• orbital manoeuvre

• "轨道"英文翻译    track; pathway; rail; runway ...
• "机动"英文翻译    motor-driven; motorized flex ...
• "轨道机动车" 英文翻译 :    rail car; railway motor car
• "变换轨道机动" 英文翻译 :    orbit-changing maneuver
• "轨道机动系统" 英文翻译 :    orbital maneuvering system (oms); orbitalmaneuveringsystemoms
• "横向轨道机动" 英文翻译 :    lateral orbital maneuver
• "引入轨道机动" 英文翻译 :    orbit insertion maneuver
• "铁道机动车" 英文翻译 :    rail motor car; railroad motor car
• "修正弹道机动" 英文翻译 :    correction maneuver
• "轨道机械化维修" 英文翻译 :    mechanized track maintenance
• "轨道平面机动" 英文翻译 :    in-plane maneuver
• "轨道修正机动" 英文翻译 :    orbit-trimming maneuver
• "轨道中段机动" 英文翻译 :    midcourse maneuver
• "改变轨道倾角机动" 英文翻译 :    dogleg maneuver
• "轨道中段修正机动" 英文翻译 :    midcourse trajectory correction maneuver
• "空间轨道末段机动" 英文翻译 :    terminal space maneuver
• "对接和轨道转移机动" 英文翻译 :    docking and transfer maneuver
• "改变轨道平面的机动" 英文翻译 :    orbital plane change maneuver; plane-change maneuver
• "改变轨道平面的机动能力" 英文翻译 :    plane-change maneuverability
• "小加速变轨道会合机动" 英文翻译 :    low-acceleration rendezvous maneuver
• "搬道机" 英文翻译 :    track shifter
• "拨道机" 英文翻译 :    mechanical track aligner
• "起道机" 英文翻译 :    rail jack; track jack; track lifting jack
• "清道机" 英文翻译 :    brush machine
• "球道机" 英文翻译 :    fairway mower

• Design and simulation of satellite orbital maneuver model on stk
  的卫星轨道机动模型设计与仿真
• Once within the gravity , it needs yet couple of orbit maneuvers to get into a right position
  一旦在这个重力场内，她需要进行两次轨道机动来调整姿态。 ）
• This paper mainly discuss the problem of method and policy of spacecraft ' s large scale orbital maneuver
  论文研究了航天器大范围轨道机动的方法与策略。
• Orbital maneuver is the primary condition for satellite autonomy , and it is the basis of phase keeping , phase maneuver and rendezvous
  卫星轨道机动是卫星自治的首要条件，它是相位保持、相位机动、交会对接的基础。
• The dissertation presents a new method for orbital maneuver based on zero effort miss steering , and many problems in this method are studied
  本文提出了基于零控流型的卫星轨道机动方法，并对此方法所涉及的具体问题进行了研究。
• Finally , this paper tried to start a new research field that named as rendezvous area and space control body , by introducing these concept , visualization for large scale orbital maneuver was able to show directly
  最后,论文尝试性的提出并研究了点对面的机动及追踪器控制体的概念,给出了高度直观的大范围轨道机动可及范围,从面的覆盖的概念上分析得到了最佳机动时限。
• According to different anticipative collisional time and maneuver occasion , author established two maneuver mathematic model , and gave the principle and occasion executing the de - orbit and de - contrail maneuver procedure . forth , author complied the orbit early warning and collision avoidance software
  根据不同的预期碰撞时刻和采取轨道机动的时机,建立了两种规避策略数学模型,并据此分析提出了两种规避方法高度分离法和轨迹分离法的原则和时机。
• Aiming at the fact that more debris collision risks are to the low earth orbit spacecraft in the getting worse debris environment , this paper gives a set of feasible debris early warning method and maneuver strategy , by means of which spacecraft can adopt orbit maneuver , evade dangerous objects so as to improve viability under the control of ground command and control center
  本论文的研究是应对日益恶化的空间碎片环境对近地航天器造成的碰撞风险,提出一套可行的碎片预警方法和规避策略,使航天器在必要时刻,通过地面的指控,采取主动的轨道机动,躲避危险物体,从而提高生存能力。
• Though the hill equation was improved it cannot satisfied with the long distance navigation . here is considering the main satellite the following satellite and the target satellite format a triangle in the space which was useful in the relative navigation . the orbit of the following satellite was resolved by calculate the hill equation
  尽管如此改进的hill方程依然不能满足远距离的相对导航,当从星在拦截目标星时,若目标星在拦截过程中发生轨道机动远离主星,这里考虑到在已知从星轨道的前提下利用主从星以及目标星在空间形成的三角关系这一有利条件进行几何法定位的研究,并通过数学仿真对其误差大小进行了分析。
• An on - line minimum - variance estimator was developed for thrust acceleration applied to orbit transfer using discrete - time radar measurements . the mass - flow - rate of propellant was selected as a state variant , which was estimated by employing an integral state model and ekf filter . the variation equations for measurement vector to mass - flow - rate have been established to linearize the discrete - time measurement equations . the algorithm has applied successfully to maneuver process in commanding satellite into geo - stationary orbit . the results show that the algorithm developed here can monitor and determine whether engine works well or failure precisely and quickly during orbit transfer process
  飞行器轨道机动过程中,为跟踪、定位机动目标和干预机动控制过程,需要统计处理离散的雷达观测量实时估计推进发动机的推力,进而确定飞行器的瞬时轨道参数.本文所述算法是该工程问题的探讨和解决方案.文章建立了轨道机动过程中连续变质量运动模型和离散雷达量测模型,推进发动机的质量秒耗量作为表征推力加速度的一个近似常量,应用扩展卡尔曼滤波对离散的雷达测量数据进行顺序统计处理给出秒耗量的最小方差估计;文章详细地推导了线性化量测模型的变分方程和观测矩阵;仿真结果表明该算法能快速、准确地估计推进发动机的质量秒耗量和向机动目标施加的实际推力