片语

high attitude maneuver大角度机动

attitude e maneuver姿态机动

unusual attitude maneuver异常姿态机动

large angle attitude maneuver大角度姿态机动的

global attitude maneuver全局姿态机动

large angle attitude maneuver control大角度姿态机动控制

rapid attitude maneuver快速姿态机动

orbital attitude and maneuver system轨道姿态与操纵系统

fast attitude maneuver姿态快速机动

英汉例句

• the rapid speed attitude maneuver based on sgcmg for small satellite is also studied.

  研究了使用sgcmg的航天器的快速姿态机动问题。

• the guidance method can meet the need of pinpoint soft landing, but its requirement for attitude change goes beyond the attitude maneuver capability of landing spacecraft.

  该制导方法虽能满足精确软着陆的需要，但对姿态变化的要求超出了着陆器姿态机动能力。

• pre-planning method based on state-space search for attitude maneuver un-der complex constraints was studied.

  研究了基于状态空间搜索的复杂约束姿态机动预先规划方法。

• the research results show that the modified guidance law can meet the need of pinpoint soft landing using the achievable attitude maneuver capability.

  研究结果表明，利用一定的姿态机动能力，修正的制导方法能够满足精确软着陆的需要。

• based on near-eigenaxis decomposition theorem of the relative attitude, the control law of relative attitude maneuver based on quaternion is designed and simulated.

  根据相对姿态的欧拉轴分解定理，设计了基于四元数反馈的相对姿态机动控制律，并对相对姿态控制律进行了仿真分析。

• the attitude maneuver path needs to plan in advance for the security of on-board sensors, which are more applied with the diversity of deep space explorer mission.

  由于深空探测器任务的多样性，星载敏感器件将越来越多，为了保证敏感器件的安全性，探测器姿态机动路径就需要进行合理的前期规划。

• this article investigates the spacecraft autonomous attitude maneuver control in the presence of forbidden attitude.

  主要研究存在禁止姿态的航天器自主姿态机动控制问题。

• to solve the attitude maneuver of a flexible satellite, this article presents a variable structure tracking control algorithm based on output feedback.

  为解决柔性航天器姿态机动的控制问题，给出了基于输出反馈的变结构跟蹤控制算法。

• in this paper, the issue on fast attitude maneuver control of a spacecraft with flexible appendix is studied.

  研究带柔性附件航天器的姿态快速机动控制问题。

• the simulation results reveal that, the large angle attitude maneuver can be accomplished by using the path replanned method and the adaptive steering law, when the sgcmg encounter partial fault.

  仿真结果表明，采用姿态机动路径重规划算法与自适应操纵律，在控制力矩陀螺部分失效的情况下，仍可以实现空间站的大角度姿态机动。

• for the satellite with rapid orbit or attitude maneuver ability, its inertia changes greatly with the fuel consumed in orbit, and consequently the mass parameters appear to be uncertain.

  具有较强变轨或姿态机动能力的卫星，在轨运行过程中其质量特性随着液体燃料的消耗而不断变化，卫星的惯量特性也随之变化，使卫星质量参数呈现不确知的特性。

• the optimal attitude maneuver problems are studied.

  研究了航天器的姿态机动最优控制问题。

• this paper deals with the near-minimum-time attitude maneuver control of vertical launching tactical missile, in order to solve fast attitude maneuver of this kind of missile.

  针对战术导弹垂直发射姿态调转时的快速性要求，研究了垂直发射快速姿态调转的次最小时间控制问题。

• this paper deals with the eigenaxis attitude maneuver of a spacecraft actuated by a control moment gyroscope (cmg) with gimbal angle constraints.

  以框架角受限的金字塔构型控制力矩陀螺（cmg）为执行机构，研究了航天器欧拉姿态机动控制问题。