转角

The attitude information consists of flight path angle and roll angle about the aircraft velocity vector axis.

这里的载体姿态信息包括关于载体飞行速度矢量轴的航迹角和伪滚转角，即伪姿态。

The result shows that the algorithm has enough precision and can satisfy the need of roll angle detection for simplified guidance for conventional ammnitions.

仿真结果表明，该解算方法具有较高的精度，基本能够满足常规弹药简易制导滚对转角探测的需要。

Then, aerodynamic parameters in different flight conditions are used to imitate the uncertainty of the system, and the digital simulation of closed-loop system designed is performed. The results show that the system can accomplish asymptotic decoupling of roll angle, sideslip angle and head-on angle for aircraft, and the system is provided with the function for restraining uncertainty in the system. This illustrates that the flight control system designed has not only good decoupling characteristic, but also better robustness.

然后用不同飞行条件下的空气动力参数变化来模拟系统的不确定性，并进行闭环系统数字仿真，结果表明，所设计的控制律不仅可实现对飞机滚转角、侧滑角、迎角等的渐近解耦控制，而且对系统不确定性具有较强的抑制作用，说明系统具有较好的解耦性和较强的鲁棒性。

The simulation results show the integrated optimization algorithm can deal with the couple and al locate the overload efficiently with the constraint of sideslip angle and roll angle.

仿真结果表明，混合优化算法能隐形地处理并联复合控制时侧向系统之间的耦合，在侧滑角和滚转角的约束下，合理地分配需用过载，提高布撒器的侧向机动能力。

The nonlinear decoupling method applied on full, hi-fidelity aircraft analysis model was unprecedented, many technique, such as disassemble-design, assemble-apply, multi-grade decoupling, were used so that the nonlinear decoupling method can be used on such a complex model. The successful design of a roll angle and overload decoupling controller show that the nonlinear decoupling is a feasible method for engineering application.

非线性解耦方法在高真实度的完整飞机系统分析模型上的应用在国内尚属，文中采用分解设计、组合应用、多级解耦控制结构等方法，解决了非线性解耦方法难于应用于复杂系统的问题，成功地设计了滚转角及过载解耦控制器，达到了较好的控制效果，为工程设计提供了新的途径。

Based on a study of the passive articulated rover,a complete suspension kinematics model from wheel to inertial reference frame is presented,which uses the D-H kinematics model method of manipulator and presentation with Euler angle of pitch,roll,and yaw.

以被动关节式地形自适应月球车为研究对象，融合关节机器人D-H坐标建模方法构建了月球车悬架运动学模型和以侧倾、俯仰和偏转角表示姿态的欧拉角方式建立了车轮到世界坐标系的悬架完整表达模型。

According to the functional requirements of adaptive front-lighting system, the relationships between the yaw angle and pitch angle of light axis in AFS and vehicle parameters, including speed, steering wheel angle and pitch angle of vehicle body are derived, thus a kinematics model for AFS is set up.

根据自适应前照灯系统的功能要求，推导了车辆参数（车速、转向盘转角和车身仰俯角）与车灯光轴沿水平和垂直两个方向的偏转角度之间的关系，建立了自适应前照灯系统的运动学模型。

The split between the two groups can hardly be papered over.

这两个团体间的分歧难以掩饰。

This approach not only encourages a greater number of responses, but minimizes the likelihood of stale groupthink.

这种做法不仅鼓励了更多的反应，而且减少跟风的可能性。