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- simulated attitude controlling 模型姿态控制
- Attitude control is obtained by gimballing the engine up to ±7 degrees. 姿态控制是由发动机摆动而得到的,摆动度最大为±7°。
- Third, multi-duty direction pattern microminiaturized attitude control module. 三是多任务指向模式的微型化姿控模块。
- The attitude control system of maneuver missile head is designed by applyi ng nonlinear decoupling control law. 然后采用非线性解耦控制理论设计了机动弹头的姿态控制系统。
- To enhance the robustness of interceptor attitude control system, a switch control method is presented to control the attitude of interceptor. 摘要为增强拦截器姿态控制系统的鲁棒性,提出了一种切换控制方法来控制拦截器的姿态。
- The Attitude Control System( ACS) software is responsible for maintaining the attitude of the spacecraft. 姿态控制系统(CS)件负责维护航空器的姿态。
- The aerocraft attitude control is divided into two parts: attitude stabilization and attitude track. 本文将飞行器姿态控制分为:姿态稳定和姿态跟踪两种情况加以研究。
- The attitude control system (ACS) ensures the satellite to keep running normally. 摘要姿态控制系统是卫星得以持续正常工作的保证。
- An attitude control law for single axial direction control of an exoatmospheric interceptor is put forward. 针对单轴定向大气层外拦截器设计了一种姿态控制律。
- The integrated power and attitude control for a bias momentum attitude control system is investigated. 研究偏置动量姿态控制系统中的集成能量与姿态控制问题。
- Flywheel is an important executive component of satellite attitude control system. 飞轮是卫星姿态控制系统的关键执行元件。
- The suspension damping control strategy for vehicle attitude control system is presented. 提出了车辆姿态控制系统的悬架阻尼控制策略。
- Affected by unsteady atmosphere disturbance,attitude control and navigation for MAV flight must be unconventional. 针对在非定常大气扰动作用下,微型飞行器MAV姿态稳定控制与导航都不同于常规的问题。
- During blastoff of the stratospheric airship by buoyancy, stable attitude control is needed. 摘要平流层飞艇在靠浮力升空的过程中,需要对其进行姿态稳定控制。
- This paper mainly studies yaw angle estimation and attitude control of Tracking and Data Relay Satellite(TDRS). 本文主要研究了中继卫星的偏航角估计和姿态控制问题。
- The improvement of flywheel control system is spurred by high performance satellite attitude control system. 提高飞轮控制系统的性能对卫星姿态控制系统具有重要意义。
- This dissertation studies the applications of backstepping control design method on spacecraft attitude control system. 本论文研究退步控制设计方法在航天器姿态控制系统中的应用问题。
- A.Kawaji, F.Arai, and T.Fukuda, “3D attitude control system for bio-micromanipulation,” IEEE, pp. 197-202, 2001. 陈泰成,“微组装系统影像伺服建模与测试”,国立成功大学机械工程学系论文,中华民国九十一年。
- The attitude control system(ACS) ensures the satellite to keep running normally. 姿态控制系统是卫星得以持续正常工作的保证。
- The work module of rudder was discussed and studied by simulation in side jet and aerodynamic compound control manner, the effect on guidance accuracy by control cycle of attitude control engine and action cycle of control loop was simulated. 重点对采用燃气动力/气动力复合控制方式中舵系统的工作模式进行了探讨及仿真研究,对姿控发动机控制周期及控制回路工作周期对制导精度的影响进行了初步仿真研究。