计算结果表明，所采用的控制律可以实现运载器跟随拖曳飞机的飞行航迹。
The simulating results indicate that these flight path control laws can ensure the vehicle flies following the flight track of the towing plane.
讨论了飞机的飞行轨迹和速度特征及其雷达测量，给出了飞行航迹的数学表示和图形编辑方法。
Plane's track and velocity feature together with their radar measure are discussed. Track mathematic description and graphic edit method are also given.
以涡轮和火箭冲压组合动力的工作模式以及飞行器飞行航迹角、迎角等为调参量，构造空天飞行器爬升轨迹优化流程。
The flow chart of optimizing ASP climb track is designed by adjusting some parameters of Euler angle, attack angle, turbine and rocket-ramjet combined cycle work models, etc.
但在景象匹配过程中会不可避免的会出现匹配错误、匹配精度不够等问题，为此，基于景象匹配过程中载体机动性能规律，提出了飞行航迹近似为直线的误匹配点剔除方法。
Based on the carrier maneuverability law in scene matching process, the paper presented a method for eliminating the mismatching points when the flight track was approximated to a straight line.
该方法能够在具有预先未知威胁的飞行环境中在线实时航迹规划。
This approach can be used for on line route re planning in flying environment with unknown threat.
模型综合考虑了各种影响空中目标航迹的因素，并对飞行控制人员的控制行为进行了分析。
All the factor that affected target trajectory and the control behavior of flight control staff were considered.
在正弦风切变假定下，利用计算机计算和飞行模拟器模拟研究了长周期振动频率上下的正弦波风切变对飞机着陆航迹的影响。
On the assumption that the wind shear is sinusoidal, the effects of long periodic oscillation on the landing path of an aircraft were studied by computer calculation and with flight simulator.
飞行试验数据处理结果表明，该方法对含有斑点型异值的航迹测量数据有很好的处理效果。
Data processing of flight test indicates that this method is good for the process of measurement with a series of outliers.
航迹角修正法的采用，进一步修正了规划出的飞行轨迹，从而获得了理想的飞行参考轨迹。
After adopting the correcting method of flight path Angle, flight path planned is further modified and ideal reference flight path is obtained.
针对近飞目标和交叉飞行目标的情况，点迹与航迹的关联采用了分块处理技术，并融合了目标的速度信息。
To deal with the situations of close flight and cross flight, the velocity information of targets and the method of partly processing are taken into track correlation.
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。
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.
TA最优航迹规划技术可以在很大程度上提高突防飞行器的突防概率，是实现飞行器低空突防飞行的关键技术。
The probability of low altitude penetration can be highly improved by the TF/TA optimal trajectory planning. Trajectory planning is a key technique in realizing low-altitude-penetration.
在分析多峰值函数优化问题的基础上，提出了一种基于进化计算的飞行器多航迹规划方法。
Based on the analysis of multi-modal function optimization using evolutionary computation, a new multiple routes planner for unmanned air vehicles is proposed.
提出了有动力再入打击飞行器的航迹优化方法。
A method was proposed for the trajectory optimization of prompt reentry strike vehicle.
现场装定飞行模式航迹数据，实时修正飞行轨迹，定时发送遥测、控制信号。
Flight path data was loaded on spot, and the flight orbit was revised in real time, remote measurement and control signal was sent out.
论述了航迹规划的基本要求，如导航要求、突防要求、飞行器性能要求及战略和战术要求。
The basic requirements such as navigation requirement, penetration requirement, characteristics requirement for the aircraft, and the strategic and tactic requirements are also introduced.
目前在飞行器航迹规划和航迹控制这一研究领域中，寻找飞行器最优航迹成为一个重要的研究方向。
Currently how to search for an optimal trajectory becomes an important aspect in trajectory planning and control's fields.
提出了一种在已知静态环境下利用进化计算实现多无人飞行器的分层离线协同航迹规划方法。
An evolutionary computation method is utilized to design a hierarchical and off-line path planner for multiple Unmanned Aerial Vehicles (UAV) coordinated navigation in known static environments.
为此本文研究了低可观测飞行器的航迹规划方法。
Therefore, this thesis makes a research on the route planning method of low observable aircraft.
解决了无人机在飞行过程中遇到突然出现的威胁时的航迹重规划难题，给出了应用该算法的具体步骤。
It mainly resolves the pop-up threats in route replanning, and the particular applying approach for this algorithm is presented.
拖曳系统的飞行性能是评价拖曳系统可行性的一项基本内容，而要求解拖曳系统的飞行性能，则必须解决拖曳系统中运载器的航迹控制问题。
The precondition of getting the systems performance is to solve the issue of flight path control laws of the towed vehicle in the system.
航迹规划是飞行任务规划的重要组成部分，对行就规划算法进行研究具有重要的理论和实用价值。
Flight path planning is a very important part of the mission planning system, so the research on the flight path planning algorithms is well worth both on theoretic and practical.
对一个高超声速飞行器设计了滑动模态观测器来估计攻角和航迹倾角。
A sliding mode observer is designed to estimate the Angle of attack and flight path Angle for a hypersonic vehicle.
航迹规划的目的是要利用地形和敌情等信息，规划出生存概率最大的无人飞行器突防轨迹。
Path planning is designed to make use of terrain and enemy and other information to plan out the largest survival probability penetration trajectory of Unmanned Aerial Vehicle (UAV).
针对多飞行器的协调航迹规划展开研究，提出了一种基于协同进化的多飞行器协调航迹规划算法。
The cooperative route planning problem of multiple air vehicles is studied with the proposal of a novel coevolutionary coordinative route planner.
试验结果表明，本文提出的控制算法能够保证阵风干扰情况下小型无人飞行器的航迹控制精度，同时具有良好的动态响应。
Tests confirm that the proposed method can improve the path following performance and dynamic response for the small unmanned aerial vehicle under wind disturbance.
试验结果表明，本文提出的控制算法能够保证阵风干扰情况下小型无人飞行器的航迹控制精度，同时具有良好的动态响应。
Tests confirm that the proposed method can improve the path following performance and dynamic response for the small unmanned aerial vehicle under wind disturbance.
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