| 1. | Study on attitude stabilization method of maneuver missile head
机动弹头姿态解耦控制方法研究 |
| 2. | Attitude stabilization of a rigid spacecraft with two controls
带两控制器刚体飞行器的姿态镇定 |
| 3. | Secondly , attitude stabilization control of the satellite is researched in the phase of infrared camera scanning object
第二,在红外相机扫描目标阶段,研究了星本体的姿态稳定控制问题。 |
| 4. | Finally , attitude stabilization control of the satellite and pointing precision of the payload are researched in the phase of infrared camera tracking object
第三,在红外相机跟踪目标阶段,研究了星本体的姿态稳定控制以及有效载荷的指向精度问题。 |
| 5. | 4 . the three - axis attitude stabilization system of the flexible satellite has been studied , in which three basic vibration modes of the solar array have been considered
4 、在挠性卫星动力学模型的基础上，建立了只考虑太阳帆板三阶振动模态的挠性卫星三轴姿态控制模型。 |
| 6. | 3 . the three - axis attitude stabilization of the rigid satellite has been studied . and , the influences of the external disturbances on the system stabilization have been studied
3 、设计了刚体卫星的三轴姿态稳定控制律，分析了外界干扰对刚体卫星姿态的影响和系统的稳定性。 |
| 7. | Next , the characteristics of the user satellites complex control system is that the high accuracy antenna pointing control is realized on the basis of ensuring the high accuracy attitude stabilization control of the satellite body
3 .用户星复合控制系统的特点是在保证卫星平台高精度姿态稳定控制的前提下,实现星间链路天线的高精度指向控制。 |
| 8. | This paper discusses the pid and sliding mode variable structure ( smvs ) control of the sonar array attitude stabilization system respectively and designs the digital controllers . the simulation results have been compared
本文分别研究了声纳基阵姿态稳定系统的pid控制及滑模变结构控制方法，设计了相应的控制器，针对仿真结果，比较了两者之间的优劣。 |
| 9. | At last , this paper realizes the sonar array attitude stabilization system based on the simulation circuitry and introduces the method of how to make control system with pc / 104 . the attitude stabilization system is debugged successfully .
最后，对上述声纳基阵姿态稳定系统进行了基于模拟电路的硬件实现，应用pc 104实现控制规律，并对整个系统进行调试。 |
| 10. | Through it the author made a deep study of the satellite attitude control subsystem , verified several sorts of disturbance torques and realized satellite three - axis attitude stabilization control and attitude maneuver under different conditions
本文在simulink下对卫星姿控系统作了比较深入的研究，对各种干扰力矩进行了验证，同时在不同的仿真条件下实现了卫星三轴稳定控制、姿态机动和飞轮的磁卸载。 |
