This paper aims at solving the deficiency of flight path control system of unmanned aerial vehicle (UAV).
本文研究解决现行无人机系统在航迹控制中存在的缺陷问题。
The precondition of getting the systems performance is to solve the issue of flight path control laws of the towed vehicle in the system.
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 simulating results indicate that these flight path control laws can ensure the vehicle flies following the flight track of the towing plane.
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 disadvantages of normal aircraft in flight path control can be overcome by using direct force control, and some new motion modes can be realized.
采用直接力控制可弥补常规飞机在轨迹操纵方面的不足，并产生某些新的运动模式。
The disadvantages of normal aircraft to realize flight path control can be overcome by using direct force control, and some new motion modes can be created.
采用直接力控制可弥补常规飞机在轨迹操纵方面的不足，并产生某些新的运动模式。
However, through free-fall testing, the researchers could quantitatively measure the samara's flight dynamics and use this information to control the samara's autorotation and flight path.
然而，通过自由落体测试，研究者可以量化的测量翅果的飞行动力并且用得到的信息数据来控制翅果的自旋和飞行轨迹。
The mechanical analysis and the trimming were performed for a novel near space aircraft which uses the variation in wind speed at high altitude to control its flight path.
对一种利用高空风的风速差控制飞行轨迹的新型低能耗临近空间飞行器，进行了力学分析与配平计算。
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。
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。
Flight path data was loaded on spot, and the flight orbit was revised in real time, remote measurement and control signal was sent out.
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。
UAV target drone, which is designed to fly along a straight-line target path by directional flight control, appeared serious flight leeway phenomena in flight test.
某型无人驾驶靶机是通过定向飞行控制来实现其靶廊飞行的，但在飞行试验时却出现了比较严重的靶廊飞行偏航现象。
Finally, we design a path planner added to the autonomous control system to meet a certain extent of autonomous flight capability.
同时为了实现初级的自主控制，考虑到飞行器的特点，设计了路径规划控制系统，使系统具有一定的程度的自主能力。
Finally, we design a path planner added to the autonomous control system to meet a certain extent of autonomous flight capability.
同时为了实现初级的自主控制，考虑到飞行器的特点，设计了路径规划控制系统，使系统具有一定的程度的自主能力。
应用推荐