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- pitch attitude control 俯仰姿态控制
- When the desired attitude is reached, the elevators are faired and the air-plane maintains the new pitch attitude. 当达到希望的姿态时，升降舵再成流线型，飞机保持新的俯仰姿态。
- 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°。
- Moving the elevators out of their faired position causes the airplane to change the pitch attitude about the lateral axis. 移动升降舵离开它们的流线型位置，使得飞机改变水平轴上的俯仰姿态。
- 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。
- This prevents the airplane slinking away from the pitch attitude you want if your attention is diverted from the instrument panel. 这防止飞机潜逃您要的沥青态度如果您的注意被牵制免受仪表盘。
- If you don't have a trim button on your joystick, you can use two keys on the number pad to trim the airplane for the proper pitch attitude. 如果您没有修剪按钮在您的控制杆, 您能使用二把钥匙在数字垫整理飞机为适当的沥青态度。
- 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。
- pitch attitude protection [THETA PROT] 俯仰姿态防护
- 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。
