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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 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。
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。
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。
Abstract ：The problems concerning an aerospace vehicle’s (ASV) atmospheric reentry flight attitude control system were researched. 摘要：研究了空天飞行器(ASV)再入跨大气层飞行时的姿态控制问题。
The stratospheric nacelle attitude control system is the key technology in keeping position stabilization and posture adjustment. 摘要气球吊篮姿态控制系统是吊篮在空中保持姿态稳定、进行姿态调整的关键部件。
Then,the interceptor has to maneuver with large angles and in this time the attitude control system is a nonlinear,MIMO,coupled system. 在这种情况下，拦截器必须进行大角度姿态机动。这时的姿态控制系统是一个非线性、多输入多输出耦合控制系统。
A large flexible vehicle with tank using reaction jet attitude control system(ACS) design is a very complex and important problem. 通过数学仿真表明,形状输入法和合理的脉冲调宽逻辑可以有效抑制大挠性飞行器姿态机动控制过程中的挠性振动。
During the early stage of reusable launch vehicle(RLV) re-entry flight,reaction control system(RCS) is a major attitude control device. 可重复使用航天器再入过程初期,反作用力控制系统是其姿态控制的主要手段,结合气动舵面可以减小飞行器对该系统的总冲需求,提高飞行器动态响应特性。
The problems concerning an aerospace vehicle's (ASV) atmospheric reentry flight attitude control system were researched. 摘要研究了空天飞行器(ASV)再入跨大气层飞行时的姿态控制问题。
A novel method of fuzzy proportional-integral-differential (PID) control by GA is designed for the attitude control system of three-axis-stable mass moment missile in this paper. 摘要针对三轴稳定的质量矩导弹姿态控制系统，提出了一种基于遗传算法进行参数寻优的模糊PID控制方法。
The spacecraft attitude control system is designed via a backstepping method,considering the attitude dynamic model on conditions that flywheels are adapted as actuatoss. 研究了航天器的姿态控制问题。考虑了飞轮作为执行机构的姿态动力学模型,应用退步控制理论设计了姿态控制算法。
The proper organic combination of the CMG control loop and DM control loop is the key of the overall forming of the BST gondola attitude control system. 这也使BST采用分级控制而获得高分辨率太阳图像的科学观测成为可能。