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。
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