1)multi-body spacecraft多体航天器
1.This paper investigates the attitude tracking control of multi-body spacecraft with external disturbance torques and parameters perturbations.为了研究具有外部干扰力矩和模型不确定性的多体航天器姿态快速跟踪控制问题,基于逆系统方法和回声状态网络(echo state network,ESN),设计了鲁棒控制器,并利用Lyapunov稳定性理论证明了控制系统的渐近稳定性。
2.This paper investigates the robust control of large angle maneuver for the multi-body spacecraft with model uncertainties.研究了具有模型不确定性的多体航天器大角度机动控制问题。
3.Lagrange s equations in quasi-coordinates are used for dynamics modeling of a multi-body spacecraft consisting of a rigid center body, several flexible appendages and an antenna.针对带有多个挠性附件以及天线转动机构的卫星等多体航天器,利用伪坐标L agrange方程建立了系统的姿态动力学模型。
英文短句/例句
1.Flexible Multibody Spacecraft Dynamic Modeling and Attitude Control;挠性多体航天器动力学建模与姿态控制技术研究
2.Multidimensional Modal Analysis Method for Solving Liquid Nonlinear Sloshing Dynamics in Spacecraft Tank;航天器贮箱液体非线性晃动动力学的多维模态分析方法
3.The spacecraft saw some of Jupiter's many moons.航天器看到了木星众多卫星中的一些。
4.Real-Time Simulation of Multi-Sapcecraft Based on Ihawk System基于ihawk的多航天器实时仿真系统
5.Multi-objective Spacecraft Reliable Control Based on BMI Optimization基于BMI优化的航天器多目标可靠控制
6.celestial navigation【航海.航空】天体导航法
7.Relative Navigation for Non-cooperative Spacecraft Based on Stereo Vision基于立体视觉的非合作航天器相对导航
8.gas storage system for manned spacevehicle载人航天器气体贮存系统
9.Simulation of Celestial Scene in Shiphandling Simulator Based on Platform of OpenGL;基于OpenGL的航海模拟器中天体运动仿真
10.Analysis and Calculation on Collision Breakup Characteristics of Orbital Spacecraft在轨航天器撞击解体特性分析与计算
11.Investigation into Digital Control of Multi-Output Full-Regulated DC-DC Converter for Spacecraft航天器多路精确稳压DC-DC变换器数字控制研究
12.Design of higher-order sliding mode controller for rigid spacecraft attitude tracking maneuver刚体航天器姿态跟踪的高阶滑模控制器设计
13.Spacecraft automatic test and spacecraft test language航天器自动化测试与航天器测试语言
14.Study of Spacecrafts Multi-Fault Diagnosis Based on Neural Network;基于神经网络的航天器多故障诊断的研究
15.Dynamical decomposition modeling and control of multi-spacecraft coordinated flying多航天器协同飞行动力学分解建模与控制
16.Analysis of unsteady heat transfer of spacecraft multilayer insulation航天器多层绝热材料的非稳态传热分析
17.Classification of Remainder Material for Aerospace Relay Based on Wavelet Transform基于小波变换的航天继电器多余物材质分类
18.vehicles for space astronomical observation空间天文观测航天器
相关短句/例句
Flexible Multibody Spacecraft挠性多体航天器
1.Flexible Multibody Spacecraft Dynamic Modeling and Attitude Control;挠性多体航天器动力学建模与姿态控制技术研究
3)Multi-spacecraft多航天器
1.The research of interoperability between Multi-spacecraft has become a hot issue in the field of aerospace,the establishment of a high confidence level of the simulation system has become the issue in depth to engineering applications.多航天器间的互操作已经成为航天领域研究的热点问题,建立高置信度的仿真系统已经成为该问题向工程应用深入的关键。
4)rigid spacecraft刚体航天器
1.Nonholonomic motion planning for the attitude of rigid spacecraft with two momentum wheel actuators;带有两个动量飞轮刚体航天器的姿态非完整运动规划问题
2.In terms of this characteristic, the three-dimensional attitude control problem of the rigid spacecraft with three manipulators is discussed in the paper.利用这一特性讨论了带空间机械臂的刚体航天器三维姿态运动的控制问题。
3.For rigid spacecraft attitude tracking system with uncertain inertia matrix and external disturbances,an adaptive sliding mode approach is presented.针对存在不确定惯量矩阵和外干扰的刚体航天器姿态跟踪系统,提出了一种自适应滑模控制方法。
5)multi spacecraft system多航天器系统
1.The applications of GPS in a multi spacecraft system with kinematical restraint but no structural restraint and force action to each other are studied in this paper.研究了 GPS在一类没有结构和力约束 ,但存在运动约束的多航天器系统中的应用。
6)lift-body升力体航天器
1.The problem of optimized reentry-trajectory design for lift-body was studied.研究了升力体航天器再入大气层的弹道优化设计问题,提出了过载约束条件下再入弹道的优化设计思路,给出了最优弹道随高度变化的绕速度轴滚转角大小的计算方法。
延伸阅读
航天器航天器spacecraft见飞行器。
