The requirements of software implementation for unmanned helicopter flight control system are analyzed in the paper.
该文分析了无人直升机飞行控制系统软件实现要求。
The modern unmanned helicopter flight control system is generally composed of the flight control computer, the servo driving mechanism, the sensor, and the ground monitor control system etc.
现代无人直升机飞行控制系统一般由飞行控制计算机、伺服驱动机构、传感器、地面监测控制等分系统组成。
This thesis focuses on the design and implementation of a flight control system for a mini unmanned helicopter.
本文围绕超小型无人直升机飞行控制系统的设计与实现展开论述。
According to the flight control characteristics for unmanned helicopter, we design distributed flight control system by means of using middleware TAO and its event service mechanism.
根据无人直升机飞行控制特点，利用中间件TAO及其事件服务机制，设计了分布式飞行控制系统。
He has conducted the design work of flight control system of "M16" helicopter and automatic pilot system of the coaxial unmanned helicopter.
主持设计了“M16”型直升机的操纵系统和共轴式无人驾驶直升机的自动驾驶仪系统。
He has conducted the design work of flight control system of "M16" helicopter and automatic pilot system of the coaxial unmanned helicopter.
主持设计了“M16”型直升机的操纵系统和共轴式无人驾驶直升机的自动驾驶仪系统。
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