Thus a DSP based digital flight attitude simulator was designed.
鉴于此作者参与设计并实现了基于DSP的数字航姿模拟器。
As an application example, its application to flight attitude control system is analysed.
作为应用实例，分析了在飞行姿态控制系统中的应用。
The effect of empennage spread on flight attitude was analyzed and validated by flight test data.
本文介绍了使用双镜头狭缝摄影对某武器系统外弹道飞行姿态测试的方法及可行性分析。
An algorithm to extract flight attitude from a space vector, which was connected by two track points, was proposed.
提出了一种用飞机前后两个位置点空间连线矢量提取飞行姿态算法。
The problems concerning an aerospace vehicle's(ASV) atmospheric reentry flight attitude control system were researched.
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 data measured by magnetic sensor can be used in calculating the flight attitude of the projectile and giving the direction benchmark of firing pulse jet.
地磁传感器测量的数据不仅用于解算弹体飞行姿态，同时可通过计算给出点火脉冲发动机选择的方向基准。
Artificial horizon, an instrument of cockpit meter systems of the ACTE, is mainly used to indicate the flight attitude, such as pitching Angle and tilt Angle etc.
水平仪是飞机综合训练模拟器座舱仪表系统中用于显示飞机飞行姿态的仪表，主要完成俯仰、倾斜等指示功能。
This paper is mainly to discuss the designing and realization of a DSP based digital flight attitude simulator, including its applications in an aircraft carried radar ATE.
这篇论文主要介绍了一种基于DSP的数字航姿模拟器的设计、实现以及它在机载雷达ate中的应用。
A flight attitude planning algorithm is developed for low observable micro-satellite shields to enhance the on-orbit satellite's survivability and operational effectiveness.
为提高在轨微小卫星的使用效能及生存能力，提出一种微小卫星低可观测外形飞行姿态规划算法。
The simulative calculation results show that the improved proportional feedback control method works effectively in the flight attitude stability control of gun-launched UAV.
仿真计算结果表明，比例反馈控制方法对炮射无人机的姿态稳定控制过程实用而有效。
If the backward force is overload, the flight attitude and the safety of the armed helicopter will be affected seriously in the aerial rocket weapon system of armed helicopters.
对于武装直升机载的航空火箭武器系统，如果发射后坐力过大，将对载机的飞行姿态和安全造成严重影响。
The communication suppressing zone is introduced to evaluate the jamming capability of the UAV and a new method is proposed to calculate it while the flight attitude is facultative.
以干扰有效压制区作为无人机通信干扰能力的评估指标，提出了一种计算无人机处于任意姿态时的地面干扰有效压制区的方法。
By correcting the rotating Angle of the image based on the flight attitude of the UAV, the direction of the aerial image can be fixed to help the operator to observe and decide correctly.
通过图像旋转的原因分析，推导出普遍适用于航拍图像纠偏处理的公式；并根据无人机飞行姿态来判断航拍图像的旋转角度进而加以纠正，使航拍图像固定指北，有助于操作员正确进行图像的观察及判定。
Kind warm smile is the best form of flight attitude, easy to accept, passengers feel, and set up a good image industry, reputation, open attitude decides success or failure, overcoming all smiles.
亲切温暖的微笑就是空乘最佳态度的表现形式，易于乘客接纳，产生宾至如归之感，同时树立了行业良好形象，为企业打开声誉，态度决定成败，微笑战胜一切。
There are several factors that can influence sonic booms -- weight, size, and shape of the aircraft or vehicle, plus its altitude, attitude and flight path, and weather or atmospheric conditions.
有几个因素可以影响音爆——飞行器的重量，大小，形状以及其飞行高度，姿势和路线，还有天气或大气状况。
INNER LOOP control, For autopilot operation this is the basis control of airplane pitch and roll attitude without regard to flight path.
内环路控制，对于自动驾驶仪操作，这是无关飞行航道的飞机俯仰姿态和坡度的基本控制。
Finally, the dissertation designed the fuzzy PD controller of trajectory tracking, which is combined with attitude Angle controller, so that the whole flight controller is completed.
本文最后设计了直升机模糊pd轨迹跟踪控制器，与姿态角控制器相结合，完成对整个飞行控制系统的设计。
To get the data of the micro air vehicle (MAV) 's attitude in true flight, the data transmit and receive equipment is the key technology.
要实现在真实飞行情况下对微型飞行器姿态等数据的测量，数据的无线收发是其关键技术。
According to the flight mission of the different phases, the attitude control schemes were designed in the paper respectively.
根据软着陆不同阶段飞行任务的不同，分阶段提出了月球探测器的姿态控制方案。
The UAV can fly along the scheduled fight path with correct attitude by the research of the control law of portrait flight track and transverse coordinated turn.
文中通过研究无人机纵向航迹跟踪和横侧向协调转弯的控制律使得无人机可以以下确的姿态沿预定的航迹飞行。
Experiment results using a flight control platform show that the model accurately reflects the dynamic relationships between the nacelles tilting Angle and the aircraft attitude.
实验结果表明，模型有效地反映了倾转旋翼机的短舱在倾转过程中，短舱倾转角与飞机姿态之间的动态关系。
Result show: this earth magnetic field orientation sensor can be used to detect attitude of high-load rotating flight body.
结果表明：该地磁方位传感器可应用于高过载旋转飞行体的姿态测量。
The attitude control thruster (ACT) is the control component of the flight vehicle.
姿态控制推力器(act)是飞行器控制系统的执行部件。
The results shows that the overload feedback structure is better than the attitude feedback structure on the maneuverable flight control.
结果表明，过载反馈系统在再入机动飞行器的飞行控制中效果较好。
The precise detection of the relative position and attitude between spacecrafts is very important, which is the base of autonomous control for spacecraft formation-flight.
航天器间相对位置和姿态的确定是实现航天器编队飞行的重要基础。
The precise detection of the relative position and attitude between spacecrafts is very important, which is the base of autonomous control for spacecraft formation-flight.
航天器间相对位置和姿态的确定是实现航天器编队飞行的重要基础。
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