无人机自主控制的研究是无人机研究项目的关键技术之一，我国在这方面的研究在理论和工程实际上尚处于起步阶段。
The automatic flight control system of the Unmanned Aerial Vehicle is one of the critical problems, and the research on this domain is still at the beginning level.
本文主要利用常规PID控制和智能PID控制的理论来研究无人机飞行控制律的设计。
The thesis adapts traditional PID control and intelligent PID control theories to study the design of UAV's fight control law.
本文主要利用常规PID控制和智能PID控制的理论来研究无人机飞行控制律的设计。
The thesis adapts traditional PID control and intelligent PID control theories to study the design of UAV's fight control law.
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