| 1. | Simulation of the remanence moment influencing on satellite attitude control system
柔性炼钢连铸仿真调度系统及其关键技术 |
| 2. | A semi - physical real - time simulation platform for satellite attitude control system based on matlab
的卫星姿态控制半物理实时仿真平台 |
| 3. | The satellite attitude control system is modeled into a close control loop with three momentum wheels on each axis
星体姿态控制系统采用三轴稳定动量轮闭环控制模型，天线指向控制系统采用开环控制。 |
| 4. | Based on the application of a certain model satellite , a monitoring & diagnosis platform of a satellite attitude control system is developed
结合具体项目,以某卫星为应用背景,开发了卫星姿控系统监测及诊断平台。 |
| 5. | Afterward , the integated platfom based on matlab - rtlab and the application of this integrated platform for design and simulation of small satellite attitude control system were studied
然后,研究了基于matlab - rtlab的集成平台的组成和基于该平台的卫星姿控一体化开发过程。 |
| 6. | On the base of active disturbance rejection control , author use active disturbance rejection control in small satellite attitude control system and designs a two - loop active disturbance rejection attitude control system
在深入研究了自抗扰控制理论的基础上,将自抗扰控制新技术应用于主动磁控小卫星姿态控制系统中。 |
| 7. | The thesis first simply introduces the satellite attitude control system and some attitude sensors . introduces the star sensor ' s function , component and working theory , development of star sensor and its main technique
文中简单介绍了卫星姿态控制和常用的姿态敏感器，介绍了星敏感器的功能、组成和工作原理，以及星敏感器技术的发展和相关技术的研究。 |
| 8. | The research on fault diagnosis and system rebuild technology in satellite attitude control system : the intelligent and independent algorithms about fault diagnosis and system rebuild technology in satellite attitude control system are put forward
卫星控制系统故障诊断与系统重构技术研究：提出了基于联邦滤波结构的卫星姿态确定系统智能自主故障诊断与系统重构方案和算法。 |
| 9. | Moment gyroscope is implement institution of the satellite attitude control system . the dynamics equation of single gimbal control moment gyroscope is set up , the control law of moment gycroscope is designed and the distribute matrix is confirmed reasonly
选择力矩陀螺作为该卫星控制系统的执行机构,建立单框力矩陀螺的动力学方程,在此基础上进行力矩陀螺控制律设计,合理地确定力矩陀螺的分配矩阵。 |
| 10. | In order to study small satellite attitude control system , the author first establishes the small satellite dynamics , kinematic models , and gives the theories of the quarternion , then study in - depth of the principles of the active magnetic control
为研究主动磁控小卫星姿态控制系统,首先建立了主动磁控小卫星动力学、运动学模型,并给出了姿态四元数的相关理论。从地磁场模型出发,深入研究了主动磁控的原理。 |
