引言随着全球化进程的推进,无人机（UAV,Unmanned Aerial Vehicles）作为现代战争＂尖兵之翼＂已在日益严峻的世界战争格局中崭露头角,其应用领域也开始多元化过渡发散。飞行控制系统（Flight Control System,简称FCS）作为无人机系统...引言随着全球化进程的推进,无人机（UAV,Unmanned Aerial Vehicles）作为现代战争＂尖兵之翼＂已在日益严峻的世界战争格局中崭露头角,其应用领域也开始多元化过渡发散。飞行控制系统（Flight Control System,简称FCS）作为无人机系统的＂大脑＂,是执行无人机自主导航、飞行控制、任务管理的成败关键所在。展开更多
In this paper, we conduct research on the unmanned aerial vehicle adaptive control system based on fuzzy control and chaosmechanics. Four rotor aircraft is a kind of nonlinear systems with underactuated, strong coupli...In this paper, we conduct research on the unmanned aerial vehicle adaptive control system based on fuzzy control and chaosmechanics. Four rotor aircraft is a kind of nonlinear systems with underactuated, strong coupling characteristic. Although in existing research,through the design of the control algorithm effectively inhibits both for fl ight control effect, but not fundamentally eliminate the effect of aircraft.Dynamic model of unmanned helicopter fl ight control system design is very approximate, need to gradually improve the modeling accuracy, soas to get the exact autonomous fl ight control, so you need to practice constantly required to modeling in the fl ight information, so the unmannedhelicopter fl ight control system to have the ability to retrieve information modeling. This paper proposes the new idea on the issues that will bemeaningful.展开更多
文摘引言随着全球化进程的推进,无人机（UAV,Unmanned Aerial Vehicles）作为现代战争＂尖兵之翼＂已在日益严峻的世界战争格局中崭露头角,其应用领域也开始多元化过渡发散。飞行控制系统（Flight Control System,简称FCS）作为无人机系统的＂大脑＂,是执行无人机自主导航、飞行控制、任务管理的成败关键所在。
文摘In this paper, we conduct research on the unmanned aerial vehicle adaptive control system based on fuzzy control and chaosmechanics. Four rotor aircraft is a kind of nonlinear systems with underactuated, strong coupling characteristic. Although in existing research,through the design of the control algorithm effectively inhibits both for fl ight control effect, but not fundamentally eliminate the effect of aircraft.Dynamic model of unmanned helicopter fl ight control system design is very approximate, need to gradually improve the modeling accuracy, soas to get the exact autonomous fl ight control, so you need to practice constantly required to modeling in the fl ight information, so the unmannedhelicopter fl ight control system to have the ability to retrieve information modeling. This paper proposes the new idea on the issues that will bemeaningful.
