1) Solar sail spacecraft
太阳帆航天器
1.
Solar sail spacecraft which is composed of four parts-sail film,structural booms,control boom,reaction wheel,and payload mass was studied.
针对由控制杆、反作用飞轮、有效载荷和太阳帆所组成的太阳帆航天器多体系统,从物理模型出发,利用拉格朗日方程建立了多体航天器的姿态动力学模型。
2.
A solar sail spacecraft which is composed of four parts-sail film,structural booms,and payload mass,control vanes was studied.
针对由有效载荷、太阳帆和4个控制叶片所组成的太阳帆航天器系统,从物理模型出发,利用欧拉方程建立了姿态动力学模型,并通过数值仿真对太阳帆航天器基于控制叶片的对日定向性能进行了研究。
3.
Dynamic model of solar sail spacecraft was established using Euler Equation.
针对由太阳帆薄膜、结构杆、有效载荷和四个控制叶片所组成的太阳帆航天器系统,从物理模型出发,利用欧拉方程建立了姿态动力学模型。
2) Solar array
太阳帆板
1.
This paper briefly reviews papers presented in the conference The papers cover 9 topics including on-orbit investigation, models and computer simulation,solar arrays and discharge phenomena,solar array test,interaction with charging environment,electric propulsion,interaction with plasma, internal charging,and material characterizations.
会议论文共涉及9个专题:飞行试验研究;模型和计算机仿真;太阳帆板和放电现象;太阳电池阵试验:与带电环境相互作用;电推进;等离子体相互作用;内带电;材料特性。
2.
The optimal control problem of the attitude of a spacecraft during the stretching process of its solar array is discussed in this paper.
讨论航天器太阳帆板伸展过程中航天器姿态运动的最优控制问题。
3.
The behavior of the satellites and their flexible solar arrays are imitated on the single axis gas bearing turntable (SAGBT) and flexible beam separately.
用单轴气浮台和挠性梁分别模拟卫星本体和太阳帆板。
3) Solar sail
太阳帆
1.
Optimal trajectory design of solar sail transfer to halo orbits;
飞向Halo轨道的太阳帆航天器轨迹优化设计
2.
Optical performance evolution of solar sail-driven lunar probe;
探月飞行中太阳帆航天器帆面光学性能演化
3.
Current status of solar sail propulsion and analysis of its key techniques;
太阳帆推进技术研究现状及其关键技术分析
4) solar panel substrate
太阳帆板
1.
A solar panel substrate planeness non contact system is presented, which employs optical triangulation method and bases on virtual precise benchmark.
介绍了一种采用斜光学三角形测量结构和基于虚拟精密测量基准的太阳帆板平面度无接触测量系统 。
5) Solar panel
太阳帆板
1.
Dynamics simulation of deployment for solar panels with hinge clearance
含铰间间隙太阳帆板展开动力学仿真
2.
The dynamics virtual prototype model of deployment of solar panels was built on ADAMS.
在ADAMS软件平台上建立了航天器太阳帆板展开过程动力学虚拟样机模型,研究了目前航天器太阳帆板典型的三种布局安装方式,分别为太阳帆板安装在航天器一侧同步展开;太阳帆板安装在航天器两侧同步展开;太阳帆板安装在四侧同步展开。
3.
The mathematic model for combined spacecraft’s solar panel obscuration was proposed based on geometry method, combined spacecraft self-body and solar panel as obscuring objects were taken into account.
太阳帆板的遮挡分析是航天器电源分系统方案设计的基础。
6) solar panel substrate
太阳能帆板
1.
Study on image processing method of light spot in planeness measurement system of solar panel substrate;
太阳能帆板平面度测量系统中光斑图像处理方法研究
2.
Based on the extended Hamilton principle, the vibration equation of the solar panel substrate modal containing several PZT actuators is derived.
太阳能帆板是给航天器提供能源的重要装置,以压电陶瓷为做动器的智能结构可以有效地抑制卫星太阳能帆板在太空中的振动。
补充资料：太阳帆航天器
太阳帆航天器，用八个三角帆叶片，每片长16、5码，用火箭搭载，送入太空。再安装上abl高能化学氟碘激光器和光束控制系统，对来袭的“猎鹰”进行拦截，而光束控制系统用来感知目标，选择瞄准点，将激光器对准瞄准点，abl对助推段的弹道进行探测和跟踪，并利用高能激光束将其击毁。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条