The flight mechanism of birds and big insects was probed valuably, and airframe dynamics and airfoil aerodynamics of Flapping Wing Micro Aerial Vehicle (FWMAV) were researched.
对鸟和昆虫的飞行机理进行了有价值的探讨，并对扑翼式微型飞行器机体动力学和机翼空气动力学进行了详细的分析。
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。
As micro flapping flight is investigated further, its control is paid more attention to.
随着微扑翼飞行器研究的不断深入，对其控制问题研究已引起了人们的重视。
The work focuses on an application and realization of embedded micro-controller LPC2138 in flight control system for aerial robotics.
研究了基于嵌入式微控制器LPC2138的空中机器人飞行控制系统的设计与实现技术。
This dissertation proposes a flapping control mechanism to solve the flight power problems in hovering flight control of the insect-like flapping micro aerial vehicles(IFMAVs).
仿真结果验证了此操控机制可以较好地解决仅一对翼的仿昆扑翼飞行器飞行动力问题。
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。
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。
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